EP3422553A1 - Power conversion device and air conditioner - Google Patents
Power conversion device and air conditioner Download PDFInfo
- Publication number
- EP3422553A1 EP3422553A1 EP17867154.1A EP17867154A EP3422553A1 EP 3422553 A1 EP3422553 A1 EP 3422553A1 EP 17867154 A EP17867154 A EP 17867154A EP 3422553 A1 EP3422553 A1 EP 3422553A1
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- EP
- European Patent Office
- Prior art keywords
- command value
- axis
- axis current
- current command
- voltage
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P21/00—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
- H02P21/0085—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation specially adapted for high speeds, e.g. above nominal speed
- H02P21/0089—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation specially adapted for high speeds, e.g. above nominal speed using field weakening
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
- F24F11/00—Control or safety arrangements
- F24F11/70—Control systems characterised by their outputs; Constructional details thereof
- F24F11/80—Control systems characterised by their outputs; Constructional details thereof for controlling the temperature of the supplied air
- F24F11/86—Control systems characterised by their outputs; Constructional details thereof for controlling the temperature of the supplied air by controlling compressors within refrigeration or heat pump circuits
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
- H02M7/00—Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
- H02M7/42—Conversion of dc power input into ac power output without possibility of reversal
- H02M7/44—Conversion of dc power input into ac power output without possibility of reversal by static converters
- H02M7/48—Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P21/00—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
- H02P21/22—Current control, e.g. using a current control loop
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P27/00—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage
- H02P27/04—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage
- H02P27/06—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using dc to ac converters or inverters
- H02P27/08—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using dc to ac converters or inverters with pulse width modulation
- H02P27/12—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using dc to ac converters or inverters with pulse width modulation pulsing by guiding the flux vector, current vector or voltage vector on a circle or a closed curve, e.g. for direct torque control
Definitions
- the present invention relates to a power conversion device and an air conditioner.
- Patent Literature 1 which relates to a technology of weak field control for a permanent magnet synchronous motor, recites "To smoothly switch between vector control featuring a current command calculation unit and voltage phase operation type weak field control, and to improve the efficiency in switching" and "The problem is solved by any one of followings or combination of them.
- a step is provided for reducing a voltage phase acquired from intermediate voltage command values V dc * and V qc * when switching from normal control to voltage phase operation type weak field control.
- a value acquired by averaging d-axis current detection values is taken as a first d-axis current command value to be input in a d-axis current command calculation unit when returning to the normal control from the voltage phase operation type weak field control. 3.
- the gain of the d-axis current command calculation unit is switched when returning to the normal control from the voltage phase operation type weak field control. 4.
- a motor constant (resistance, inductance, power generation constant) identification calculation unit is provided in addition to the normal control and voltage phase operation type weak field control.
- Patent Literature 1 Japanese Patent Application Publication No. 2010-142030
- AC voltage from, for instance, a commercial power source is converted to DC voltage by using a converter circuit; the DC voltage is further converted to AC voltage with each given frequency by an inverter device; and the AC voltage is used to drive a permanent magnet synchronous motor (hereinafter, referred to as a "motor").
- a motor permanent magnet synchronous motor
- the DC voltage output from the converter circuit has convoluted ripple components.
- the ripple components of the DC voltage may cause an ON/OFF state of weak field control to be switched frequently. This switching induces distortion in the output voltage or current of the inverter device, thereby making the motor unstable. This may cause problems such as a stoppage due to overcurrent, malfunctions, a rapid change in the rotation speed.
- the present invention has been made in view of the above-mentioned situations.
- the purpose of the present invention is to provide a power conversion device allowing for stable operation of motors and an air conditioner therewith.
- An aspect of the present invention provides a power conversion device comprising:
- the present invention enables motors to be driven stably.
- FIG. 1 is a block diagram showing the motor drive system S1 according to the first embodiment of the present invention.
- the motor drive system S1 includes: a converter circuit 2 in which AC voltage from an AC voltage source 1 is converted to DC voltage; an inverter device 3 (power conversion device); and a permanent magnet synchronous motor 4 (hereinafter, referred to as a motor 4).
- the motor 4 is provided with a rotor having permanent magnets embedded (not shown) and a stator having windings (not shown).
- the AC voltage source 1 supplies 3-phase AC voltage to the converter circuit 2.
- the converter circuit 2 includes a 3-phase diode bridge 5, a DC reactor 6, and a smoothing capacitor 7.
- the 3-phase diode bridge 5 When 3-phase AC voltage is supplied from the AC voltage source 1 to the 3-phase diode bridge 5, the 3-phase diode bridge 5 outputs full-wave-rectified voltage.
- the 3-phase diode bridge 5 outputs the voltage on the P side and the N side.
- the P side is connected to the DC reactor 6.
- the smoothing capacitor 7 is connected to the DC reactor 6 output side and the 3-phase diode bridge 5 output N side. Then, the converter circuit 2 outputs, as a DC voltage, an inter-terminal voltage of the smoothing capacitor 7.
- the DC voltage output from the converter circuit 2 is input into the inverter device 3.
- the inverter device 3 includes: a DC voltage detection circuit 8; an intelligent power module (IPM) 9 with an inverter function; a U-phase motor current detection circuit 10; a V-phase motor current detection circuit 11; a controller 12; and a gate drive circuit 13.
- IPM intelligent power module
- the DC voltage supplied from the converter circuit 2 is input into the IPM 9 (inverter).
- the IPM 9 includes 6 IGBTs and free-wheeling diodes (FWD) connected in parallel to the respective IGBTs (both are not numbered). Then, the IPM 9 converts the DC voltage to 3-phase AC voltage by switching each IGBT ON/OFF through using a gate drive signal 18 supplied from the gate drive circuit 13. This 3-phase AC voltage is an output of the inverter device 3. Meanwhile, the DC voltage detection circuit 8 measures the DC voltage input into the inverter device 3 and sends, as a DC voltage detection signal 14, the measured results to the controller 12.
- the 3-phase AC voltage output from the inverter device 3 is applied to windings of the motor 4.
- a U-phase motor current detection circuit 10 and a V-phase motor current detection circuit 11 are disposed partway through paths of a U-phase current and a V-phase current, respectively, of 3-phase current flowing through the motor 4.
- These current detection circuits 10 and 11 supply, to the controller 12, a U-phase motor current detection signal 15 and a V-phase motor current detection signal 16, respectively.
- the controller 12 Based on the DC voltage detection signal 14, the U-phase motor current detection signal 15, and the V-phase motor current detection signal 16, the controller 12 calculates a DUTY ratio so as to switch ON/OFF each IGBT in the IPM 9 and outputs a PWM signal 17 with the DUTY ratio.
- the PWM signal 17 is converted to a gate drive signal 18 having an enough voltage to switch ON/OFF each IGBT in the gate drive circuit 13.
- the controller 12 includes general computer hardware such as a CPU (central processing unit), a RAM (random access memory), and a ROM (read only memory).
- the ROM stores, for example, a control program executed by the CPU and various data.
- FIG. 2 is a block diagram showing an algorithm of the controller 12 and illustrates functional blocks implemented by, for example, the control program.
- the U-phase motor current detection signal 15 and the V-phase motor current detection signal 16 are input into an A/D converter 19. Then, the A/D converter 19 outputs, as a U-phase current detection value Iu and a V-phase current detection value Iv, the resulting values as obtained by multiplying the U-phase motor current detection signal 15 and the V-phase motor current detection signal 16 by corresponding predetermined gains (referred to as current detection circuit gains).
- a dq converter 20 receives the U-phase current detection value Iu, the V-phase current detection value Iv, and a d-axis phase ⁇ dc (its details are described below). Then, the dq converter 20 outputs a d-axis current detection value I dc and a q-axis current detection value I qc calculated based on the following [Expression 1].
- a coordinate system is assumed that rotates at the electrical angle of the motor 4 (value obtained by multiplying a mechanical angle by the number of pole pairs of the motor 4).
- a d-axis is set to the direction of a magnetic flux generated by the permanent magnets
- a q-axis is set to an axis perpendicular to the d-axis.
- the coordinate system having the d-axis and the q-axis is called a "dq-axis coordinate system".
- the above-mentioned d-axis current detection value I dc and q-axis current detection value I qc are values of the dq-axis coordinate system.
- an axis error calculator 21 receives the d-axis current detection value I dc , the q-axis current detection value I qc , and an inverter frequency ⁇ 1 . Then, the axis error calculator 21 calculates and outputs an axis error ⁇ c based on the following [Expression 2]. Note that in [Expression 2], V d * is a d-axis voltage command value; V q * is a q-axis voltage command value; R is resistance of the windings of the motor; L d is motor d-axis inductance; and L q is motor q-axis inductance.
- ⁇ ⁇ c tan ⁇ 1 V d * ⁇ R ⁇ I dc + ⁇ 1 ⁇ L q ⁇ I qc / V q * ⁇ R ⁇ I qc ⁇ ⁇ 1 ⁇ L q ⁇ I dc
- a PLL control unit 22 uses the axis error ⁇ c as an input and executes proportional integral control to calculate the inverter frequency ⁇ 1 .
- a d-axis phase updating unit 23 adds, to the previous output value (before 1 calculation cycle) of a d-axis phase ⁇ dc , a value ⁇ dc obtained by dividing the inverter frequency ⁇ 1 by that at the previous calculation cycle. Then, the d-axis phase updating unit 23 outputs the added value as a current value for the d-axis phase ⁇ dc .
- a speed control unit 24 calculates a deviation ⁇ (not shown) between an inverter frequency command value ⁇ 1 * (frequency command value) and the inverter frequency ⁇ 1 , and executes proportional integral control based on the deviation ⁇ to calculate a q-axis current command value I q *.
- a current control unit 25 calculates a deviation ⁇ I q (not shown) between the q-axis current command value I q * and the q-axis current detection value I qc , and executes proportional integral control using the deviation ⁇ I q as an input to calculate a q-axis current command correction amount (not shown).
- the current control unit 25 outputs, as a second q-axis current command value I q **, a value obtained by adding the q-axis current command correction amount to the q-axis current command value I q *.
- the current control unit 25 executes proportional integral control using, as an input, a deviation ⁇ I d (not shown) between the d-axis current command value I d * and the d-axis current detection value I dc , and then outputs the resulting value as a second d-axis current command value I d **.
- a V d V q calculator 26 receives the inverter frequency command value ⁇ 1 *, the second q-axis current command value I q **, and the second d-axis current command value I d **, and calculates a d-axis voltage command value V d * and a q-axis voltage command value V q * by using the following [Expression 3].
- K e is an induced voltage constant of the motor 4.
- An AVR (automatic voltage regulator; voltage correction) calculator 27 receives the d-axis voltage command value V d * and the q-axis voltage command value V q * and calculates a motor voltage phase ⁇ based on [Expression 4].
- ⁇ ⁇ tan ⁇ 1 ⁇ V d * V q *
- V 1 V d * ⁇ sin ⁇ ⁇ + V q * ⁇ cos ⁇ ⁇
- the AVR calculator 27 calculates a DC voltage detection value V dc , which is obtained by multiplying the DC voltage detection signal 14 by a predetermined gain (referred to as a DC voltage detection circuit gain), and then calculates a motor voltage modulation rate K hV1 based on [Expression 6].
- K h V 1 2 ⁇ V 1 V dc
- the AVR calculator 27 calculates and outputs a d-axis voltage modulation rate K hVd and a q-axis voltage modulation rate K hVq based on [Expression 7].
- ⁇ weak is a weak field control voltage-manipulating variable.
- K hVd K hV 1 ⁇ sin ⁇ ⁇ + ⁇ ⁇ weak
- K hVq K hV 1 ⁇ cos ⁇ ⁇ + ⁇ ⁇ weak
- a dq inverter unit 28 receives the d-axis voltage modulation rate K hVd , the q-axis voltage modulation rate K hVq , and the d-axis phase ⁇ dc , and outputs a U-phase voltage modulation rate Khvu, a V-phase voltage modulation rate KhVv, and a W-phase voltage modulation rate K hVw based on [Expression 8].
- the "weak field control” refers to the feature of controlling phases of the d-axis and q-axis voltage modulation rates K hVd and K hVq based on [Expression 7] and then generating, in the windings of the motor 4, a magnetic flux that weakens a magnetic flux generated by the permanent magnets.
- the weak field control voltage-manipulating variable is 0, the magnetic flux that weakens the magnetic flux generated by the permanent magnets may be induced by controlling the d-axis current command value I d *. This operation may be similar to the weak field control, but is not called the "weak field control" in this embodiment and the additional embodiments.
- the modulation processing unit 29 modulates the U-, V-, and W-phase voltage modulation rates Khvu, KhVv, and Khvw by using a triangular wave-like modulating signal MD, and outputs post-modulation U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and K hVw '.
- the post-modulation U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and Khvw' are expressed in [Expression 9].
- K hVu ′ K hVv ′ K hVw ′ K hVu K hVv K hVw ⁇ max K hVu , K hVv , K hVw + min K hVu , K hVv , K hVw 2 .
- FIG. 3 is a waveform diagram showing a pre-modulation U-phase voltage modulation rate K hVu , a modulating signal MD, and a post-modulation U-phase voltage modulation rate K hVu '. Note that a corresponding V-phase signal is delayed 120 degrees from the U-phase signal and a corresponding W-phase signal is delayed 240 degrees from the U-phase signal (not shown).
- the utilization rate of the DC voltage detection value V dc improves.
- the output voltage of the inverter device is increased by maximum 15%.
- the modulation processing unit 29 executes upper and lower limit processing. Specifically, the upper limit and the lower limit of the output value are restricted to 1 and -1, respectively.
- a PWM signal converter 30 compares how large or small the carrier signal CR is relative to the U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and Khvw', and then outputs a PWM signal 17.
- the PWM signal 17 includes 6 signals: a U-phase P-side PWM signal, a U-phase N-side PWM signal, a V-phase P-side PWM signal, a V-phase N-side PWM signal, a W-phase P-side PWM signal, and a W-phase N-side PWM signal.
- FIG. 4 is waveform diagrams illustrating the PWM signals and a carrier signal CR.
- the carrier signal CR is a fixed-cycle triangular wave.
- the P-side PWM signal and the N-side PWM signal of each phase are signals where the ON/OFF state is inverted.
- the output values of the modulation processing unit 29, namely the U-, V-, and W-phase voltage modulation rates Khvu', K hVv ', and Khvw' reach the upper limit (1) or the lower limit (-1)
- the output voltage of the inverter device 3 may be saturated, causing the motor to malfunction. This may stop the motor 4.
- the weak field control unit 31 in FIG. 2 executes, when the motor voltage modulation rate K hV1 reaches 1.15, the weak field control.
- the weak field control unit 31 calculates a deviation ⁇ I q between the q-axis current command value I q * and the q-axis current detection value I qc , performs integral control using the deviation ⁇ I q as an input, and calculates a weak field control voltage-manipulating variable ⁇ weak .
- the weak field control unit 31 switches a weak field control flag FLG weak from OFF to ON.
- the flag FLG weak is a flag that designates the ON/OFF state of the weak field control.
- the weak field control unit 31, instead of the current control unit 25, is used to correct the deviation ⁇ I q between the q-axis current command value I q * and the q-axis current detection value I qc by using feedback control.
- the condition where the motor voltage modulation rate K hV1 reaches 1.15 means that the output voltage of the inverter device 3 gets saturated. This is the same as the condition where the output value (e.g., the U-phase voltage modulation rate K hVu ' shown in FIG. 3 ) of the modulation processing unit 29 reaches the upper limit (1) or the lower limit (-1).
- FIG. 5 is a diagram showing a phase relation, in the dq-axis coordinate system, among a d-axis voltage command value V d * and a q-axis voltage command value V q * at the time of weak field control and a voltage command wave high point V 1 .
- V 1 is a synthetic vector of the V d * and V q *.
- the phase of voltage applied to the motor 4 is a phase obtained by adding to the phase of Vi, namely the motor voltage phase ⁇ .
- the weak field control unit 31 switches the FLG weak to OFF.
- the integral term of the proportional integral control of the weak field control unit 31 is cleared to 0.
- the current control unit 25 resumes operation of the proportional integral control.
- the proportional integral control using the deviations ⁇ I d and ⁇ I q in the current control unit 25 is switched between stop and execution states. Because of this, if the ON/OFF state of the flag FLG weak is frequently switched, the current control unit 25 is unstably operated. Here, in this embodiment, the flag FLG weak is switched less frequently so as to stably operate the controller 12.
- the weak field change-suppressing control unit 32 (d-axis current command unit) shown in FIG. 2 .
- the DC voltage output from the converter circuit 2 may have convoluted ripple components.
- the ripple components are transferred, via the DC voltage detection signal 14, to K hV1 .
- the weak field control unit 31 switches the FLG weak from OFF to ON; and when the K hV1 decreases to 1.10, the weak field control unit 31 switches the FLGweak from ON to OFF. Due to this, the FLG weak is switched frequently when the ripple components of the K hV1 are 0.05 or more.
- the weak field change-suppressing control unit 32 adjusts the d-axis current command value I d * so as to prevent the K hV1 from fluctuating in a range from less than 1.10 to more than 1.15.
- FIG. 6 is a flow chart of a control program executed every given time in the weak field change-suppressing control unit 32.
- the low range component K hV1_fil of the motor voltage modulation rate which component is obtained after the K hV1 is subjected to low-pass filter processing, is calculated.
- Step S104 if the FLG weak is OFF ("YES" at Step S104) and the K hV1_fil is less than 1.05 or more than 1.10, the process goes to Step S112.
- the I d * is set to 0.
- FIG. 7 is a graph showing the relationship among the d-axis current command value I d *, the inverter frequency command value ⁇ 1 *, and the motor voltage modulation rate K hV1 .
- the q-axis current command value I q * is kept constant; the abscissa represents the inverter frequency command value ⁇ 1 *, which is increased; and the ordinate represents the d-axis current command value I d *, the maximum/minimum of the motor voltage modulation rate K hV1 , and the low range component K hV1_fil of the motor voltage modulation rate.
- the inverter frequency command value ⁇ 1 * increases, the low range component K hV1_fil of the motor voltage modulation rate becomes larger.
- Step S112 of FIG. 6 is executed and the d-axis current command value I d * is set to 0.
- Step S110 of FIG. 6 is executed, so that the I d * starts decreasing (the absolute value starts increasing). While the absolute value of the I d * is increased, the slope of the K hV1_fil gets less steep. As soon as the inverter frequency command value ⁇ 1 * reaches the frequency ⁇ P2 , the K hV1_fil is 1.10 or more. Then, Step S112 of FIG. 6 is re-executed. At this step, the I d * is set to 0, so that the K hV1_fil abruptly rises as shown in FIG. 7 .
- the maximum of the K hV1 is 1.15 or more and the minimum of the K hV1 is 1.10 or more as shown in FIG. 7 where ⁇ 1 * > ⁇ P2 .
- the weak field control unit 31 switches the FLG weak from OFF to ON; and when the K hV1 decreases to 1.10, the weak field control unit 31 switches the FLG weak from ON to OFF.
- the FLG weak is switched less frequently.
- Step S104 is judged as "NO” when the control program ( FIG. 6 ) is next implemented. Then, the process goes to Step S106.
- the low range component K hV1_fil of the motor voltage modulation rate is 1.05 or more and 1.15 or less is determined.
- the K hV1_fil exceeds 1.15, so that this step is judged as "NO”.
- the process goes to Step S112. Due to this, the d-axis current command value I d * is kept constant at 0.
- Step S106 is judged as "YES”.
- the d-axis current command value I d * is calculated based on [Expression 10]. Meanwhile, if the FLG weak is ON and the K hV1_fil is less than 1.05, the I d * is set to 0 at Step S110.
- FIG. 8 is a graph showing another relationship among the d-axis current command value I d *, the inverter frequency command value ⁇ 1 *, and the motor voltage modulation rate K hV1 .
- the q-axis current command value I q * is kept constant; the abscissa represents the inverter frequency command value ⁇ 1 *, which is decreased; and the ordinate represents the d-axis current command value I d *, the maximum/minimum of the motor voltage modulation rate K hV1 , and the low range component K hV1_fil of the motor voltage modulation rate.
- the K hV1_fil As the ⁇ 1 * decreases, the K hV1_fil also decreases. When the K hV1_fil becomes 1.15 or less at the frequency ⁇ P4 , the I d * decreases stepwise (the absolute value increases) and the K hV1 also decreases stepwise. This allows the maximum of the K hV1 to be less than 1.15 and the minimum of the K hV1 to be less than 1.10, so that the FLG weak is switched less frequently.
- this embodiment includes: an inverter (9) which converts supplied DC voltage (V dc ) to an AC output voltage and supplies the AC output voltage to windings, and which, in accordance with the DC voltage (V dc ), changes a saturation level at which the output voltage is saturated, in order to drive a motor (4) equipped with a stator having the windings and a rotor having permanent magnets; and a controller (12) which, when the output voltage is lower than the saturation level, increases an output current of the inverter such that a magnetic flux that weakens or strengthens a magnetic flux generated by the permanent magnets is generated in the windings.
- the controller (12) includes, when in a coordinate system that rotates at a rotation speed of the electrical angle of the motor (4), a d-axis is set to the direction of a magnetic flux generated by the permanent magnets and a q-axis is set to an axis perpendicular to the d-axis, the q-axis current command unit (24) configured to output the q-axis current command value (I q *), which is a command value for the q-axis component of the output voltage, based on the frequency command value ( ⁇ 1 *); and the d-axis current command unit (32) configured to output the d-axis current command value (I d *), which is a command value for the d-axis component of the output current, based on the frequency command value ( ⁇ 1 *), wherein the d-axis current command unit (32) controls, when the output voltage is lower than the saturation level, the d-axis current command value (I d *) such that a magnetic flux that weakens
- Steps S110 and S112 set the d-axis current command value I d *. This can prevent the flag FLG weak from being switched frequently, allowing for stable operation of the motor 4.
- the weak field change-suppressing control unit 32 executes the proportional control in [Expression 10].
- the proportional gain K of this proportional control is preferably adjusted in accordance with characteristics of the motor 4. Specifically, when the proportional gain K is too large, the d-axis current is too small (the absolute value is too large), causing a problem of increasing a loss in the motor 4 or the inverter device 3. By contrast, when the proportional gain K is too small, a problem occurs where the weak field control flag FLG weak is switched frequently.
- this embodiment is to mitigate complexities of changing the proportional gain K in accordance with the characteristics of the motor 4.
- the configuration of this embodiment is the same as of the first embodiment ( FIGS. 1 and 2 ). However, as a control program executed in the weak field change-suppressing control unit 32, used is one illustrated in FIG. 9 instead of the program according to the first embodiment ( FIG. 6 ).
- Step S122 of FIG. 9 the low range component K hV1_fil of the motor voltage modulation rate, which component is obtained after the motor voltage modulation rate K hV1 is subjected to low-pass filter processing, is calculated.
- Step S124 whether or not the K hV1_fil is 1.05 or more and 1.15 or less is determined. If this step is judged as "YES”, the process goes to Step S126 and the d-axis current command value I d * is then calculated.
- FIG. 10 is a block diagram illustrating a main section of the weak field change-suppressing control unit 32 according to this embodiment. That is, FIG. 10 depicts, as blocks, content of the d-axis current command value I d * calculation processing executed in the above Step S126.
- a low-pass filter (LPF) 40 is used to subject the motor voltage modulation rate K hV1 to low-pass filter processing so as to output the low range component K hV1_fil of the motor voltage modulation rate.
- the subtracter 42 subtracts the low range component K hV1_fil of the motor voltage modulation rate from a target value 1.05.
- An integral control unit 44 executes proportional integral control using a value after this subtraction.
- a limiter processing unit 46 executes limiter processing such that the upper limit of the output signal from the integral control unit 44 is set to 0. Then, the resulting value is output as the d-axis current command value I d *.
- Step S127 it is determined whether or not the d-axis current command value I d * is a predetermined value I d_SET or more. If this step is judged as "YES”, the process of this routine is ended.
- a d-axis current is controlled.
- Step S124 or S127 is judged as "NO”
- the process goes to Step S128 and the d-axis current command value I d * is set to 0. Then, the process of this routine is ended.
- the integral control unit 44 controls the d-axis current command value I d * so as to make the low range component K hV1_fil of the motor voltage modulation rate closer to the target value 1.05. This enables the low range component K hV1_fil of the motor voltage modulation rate to be kept almost constant (at a value at or near the target value 1.05) regardless of the characteristics of the motor 4.
- FIG. 11 is a graph showing the relationship among the d-axis current command value I d *, the inverter frequency command value ⁇ 1 *, and the motor voltage modulation rate K hV1 according to this embodiment.
- the q-axis current command value I q * is kept constant; and while the inverter frequency command value ⁇ 1 * is increased, indicated are the d-axis current command value I d *, the maximum/minimum of the motor voltage modulation rate K hV1 , and the low range component K hV1_fil of the motor voltage modulation rate.
- Step S124 (see FIG. 6 ) is then judged as "YES”. Subsequently, Step S126 is executed, so that even if the inverter frequency command value ⁇ 1 * is then increased, the K hV1_fil stays at almost 1.05.
- the frequency ⁇ P21 is set to the inverter frequency command value ⁇ 1 * where the low range component K hV1_fil of the motor voltage modulation rate reaches 1.05.
- the K hV1_fil of the motor voltage modulation rate While the low range component K hV1_fil of the motor voltage modulation rate is kept at the target value 1.05, the I d * decreases (the absolute value increases) as the ⁇ 1 * increases. Because the absolute value of the I d * is increased, the K hV1_fil is kept constant. The condition where the low range component K hV1_fil of the motor voltage modulation rate is kept constant is the same as the condition where the output voltage of the inverter device 3 is kept substantially constant.
- Step S128 of FIG. 9 is re-executed and the d-axis current command value I d * is thus set to 0. Due to this, the K hV1_fil abruptly rises.
- the frequency ⁇ P22 is set to the inverter frequency command value ⁇ 1 * at the timing of the abrupt rise.
- the weak field control unit 31 switches the FLG weak from OFF to ON; and when the K hV1 decreases to 1.10, the weak field control unit 31 switches the FLG weak from ON to OFF.
- the weak field control flag FLG weak is kept ON, so that the FLG weak is switched less frequently.
- the predetermined value I d_SET is a value at which various defects may occur after the I d * is decreased to that value or less, and should be adjusted in accordance with the characteristics of the motor 4.
- FIG. 12 is a graph showing another relationship among the d-axis current command value I d *, the inverter frequency command value ⁇ 1 *, and the motor voltage modulation rate K hV1 according to this embodiment.
- the q-axis current command value I q * is kept constant; and while the inverter frequency command value ⁇ 1 * is decreased, indicated are the d-axis current command value I d *, the maximum/minimum of the motor voltage modulation rate K hV1 , and the low range component K hV1_fil of the motor voltage modulation rate.
- the K hV1_fil As the ⁇ 1 * decreases from the depicted maximum, the K hV1_fil also decreases.
- the I d * decreases stepwise (the absolute value increases) and the K hV1_fil also decreases stepwise to the target value 1.05.
- the maximum of the motor voltage modulation rate K hV1 is less than 1.15 and the minimum is less than 1.10. This permits the flag FLG weak to be switched OFF by the weak field control unit 31. This OFF state stays continuously. Because of the above, The FLG weak is switched less frequently.
- the d-axis current command unit (32) controls the d-axis current command value (I d *) such that the output voltage is kept substantially constant while the frequency command value ( ⁇ 1 *) changes. More specifically, based on the low range component K hV1_fil of the motor voltage modulation rate, the d-axis current command value I d * is set in Steps S126 and S128. This, like the first embodiment, can prevent the flag FLG weak from being switched frequently. Besides, the d-axis current command value I d * can be set without using [Expression 10] (without using the proportional gain K). Hence, it is possible to mitigate complexities of setting the proportional gain K in accordance with the characteristics of the motor 4.
- the predetermined value I d_SET has been adjusted in accordance with the characteristics of the motor 4. In this embodiment, this adjustment is unnecessary, and it is possible to mitigate complexities of changing various parameters in accordance with the characteristics of the motor 4.
- the configuration of this embodiment is similar to that of the first embodiment ( FIGS. 1 and 2 ), but the algorithm of the controller 12 differs from that of the first embodiment ( FIG. 2 ).
- FIG. 13 is a block diagram illustrating a main section of the algorithm of the controller 12 according to this embodiment. Note that in the description below, elements corresponding to the respective elements of FIGS. 1 to 12 have the same reference numerals so as to avoid redundancy.
- the configuration of the controller 12 according to this embodiment is substantially the same as of the first embodiment (see FIG. 2 ). However, a current control unit 33 shown in FIG. 13 is used as an alternative for the current control unit 25 shown in FIG. 2 .
- the controller 12 according to this embodiment includes an adder 35, a V d V q controller 36, and an AVR calculator 37.
- the current control unit 33 includes subtracters 331 and 333, proportional integral control units 332 and 334, and an adder 335.
- the subtracter 331 subtracts a d-axis current detection value I dc from 0.
- the integral control unit 332 executes proportional integral control using a value (-I dc ) after this subtraction, and the resulting value is output as a second d-axis current command value I d **.
- the proportional integral control unit 332 stops its operation when the low range component K hV1_fil of the motor voltage modulation rate is 1.05 or more. At this time, the integral term is not cleared to 0 and the value is held.
- the adder 35 adds the d-axis current command value I d * and the second d-axis current command value I d **. Based on the second q-axis current command value I q **, the resulting value (I d * + I d **) added by the adder 35, and the inverter frequency command value ⁇ 1 *, the VdVq calculator 26 calculates d-axis and q-axis voltage command values V d * and V q *. Specifically, instead of the "I d **" in the above [Expression 3], the "I d * + I d **" is used to give the d-axis and q-axis voltage command values V d * and V q *.
- the V d V q calculator 36 calculates a d-axis voltage-determining value V d_SET and a q-axis voltage-determining value V q_SET .
- the d-axis and q-axis voltage command values V d * and V q * in [Expression 3] according to the above first embodiment correspond to the d-axis and q-axis voltage-determining values V d_SET and V q_SET according to this embodiment, respectively.
- the AVR calculator 27 calculates, like calculations using the above [Expression 4], [Expression 5], and [Expression 6], the motor voltage modulation rate K hV1 .
- the d-axis and q-axis voltage command values V d * and V q * are replaced by the d-axis and q-axis voltage-determining values V d_SET and V q_SET and the motor voltage modulation rate K hV1 is replaced by the motor voltage modulation rate-determining value K hV1_SET .
- the AVR calculator 37 uses the resulting Expressions to calculate the motor voltage modulation rate-determining value K hV1_SET .
- the motor voltage modulation rate K hV1 and the motor voltage modulation rate-determining vale K hV1_SET as so calculated are sent to the weak field change-suppressing control unit 32.
- the weak field change-suppressing control unit 32 calculates the d-axis current command value I d * by using the algorithm shown in FIG. 10 . The following describes, in detail, processing of this weak field change-suppressing control unit 32.
- FIG. 14 is a flow chart of a control program executed in the weak field change-suppressing control unit 32 according to this embodiment instead of the first embodiment ( FIG. 6 ).
- the low range component K hV1_fil of the motor voltage modulation rate which component is obtained after the K hV1 is subjected to low-pass filter processing, is calculated.
- the low range component K hV1_SETfil of the motor voltage modulation rate-determining value which component is obtained after the K hV1_SET is subjected to low-pass filter processing, is calculated.
- Step S134 when the process goes to Step S134, whether or not the K hV1_SETfil is 1.05 or more and 1.15 or less is determined. If this step is judged as "YES”, the process goes to Step S136 and the weak field change-suppressing control unit 32 uses the algorithm shown in FIG. 10 to calculate the d-axis current command value I d *. If Step S134 is judged as "NO”, the process goes to Step S138 and the weak field change-suppressing control unit 32 sets the d-axis current command value I d * to 0.
- FIG. 15 is a graph showing another relationship among the d-axis current command value I d *, the inverter frequency command value ⁇ 1 *, and the motor voltage modulation rate K hV1 according to this embodiment.
- the q-axis current command value I q * is kept constant; and while the inverter frequency command value ⁇ 1 * is increased, indicated are the d-axis current command value I d *, the maximum/minimum of the motor voltage modulation rate K hV1 , the low range component K hV1_fil of the motor voltage modulation rate, and the low range component K hV1_SETfil of the motor voltage modulation rate-determining value.
- the K hV1_fil of the motor voltage modulation rate becomes larger.
- the K hV1_fil is, for a while, kept at almost the target value 1.05.
- the I d * decreases (the absolute value increases).
- the frequency ⁇ P31 (first command value) is set to the inverter frequency command value ⁇ 1 * where the K hV1_fil arrives at 1.05.
- the low range component K hV1_SETfil of the motor voltage modulation rate-determining value is not affected by the d-axis current command value I d *.
- the K hV1_SETfil continuously increases as the inverter frequency command value ⁇ 1 * increases.
- Step S138 of FIG. 14 is executed and the d-axis current command value I d * is thus set to 0. Then, the low range component K hV1_fil of the motor voltage modulation rate abruptly rises.
- the frequency ⁇ P32 (second command value) is set to the inverter frequency command value ⁇ 1 * at the timing of the abrupt rise.
- the weak field control unit 31 switches the FLG weak from OFF to ON; and when the K hV1 decreases to 1.10, the weak field control unit 31 switches the FLG weak from ON to OFF.
- the weak field control flag FLG weak is kept ON, so that the FLG weak is switched less frequently.
- the d-axis current command unit (32) sets, if the frequency command value ( ⁇ 1 *) is less than the first command value ( ⁇ P31 ), the d-axis current command value (I d *) to 0; increases, if the frequency command value ( ⁇ 1 *) is the first command value ( ⁇ P31 ) or more and less than the predetermined second command value ( ⁇ P32 ), the absolute value of the d-axis current command value (I d *) as the frequency command value ( ⁇ 1 *) becomes larger, so as to keep the output voltage substantially constant; and sets, if the frequency command value ( ⁇ 1 *) is the second command value ( ⁇ P32 ) or more, the d-axis current command value (I d *) to 0.
- the d-axis current command value I d * is set in Steps S136 and S138. This, like the first embodiment, can prevent the flag FLG weak from being switched frequently. Further, the d-axis current command value I d * can be set without using the predetermined value I d_SET . Hence, it is possible to mitigate complexities of setting the predetermined value I d_SET in accordance with the characteristics of the motor 4.
- the configuration of this embodiment is similar to that of the first embodiment ( FIG. 1 ), but the algorithm of the controller 12 differs from that of the first embodiment.
- FIG. 16 is a block diagram showing the algorithm of the controller 12 and illustrates functional blocks implemented by, for example, the control program. Note that in the description below, elements corresponding to the respective elements of FIGS. 1 to 15 have the same reference numerals so as to avoid redundancy.
- the controller 12 has a low-pass filter 54.
- the low-pass filter 54 is used to subject the motor voltage modulation rate K hV1 to low-pass filter processing so as to output, to the weak field control unit 31, the resulting value as the low range component K hV1_fil2 of the motor voltage modulation rate.
- the time constant of the low-pass filter 54 is sufficiently larger than the ripple frequency of the DC voltage detection value V dc .
- the flag FLG weak when the weak field control flag FLG weak is OFF and the motor voltage modulation rate K hV1 reaches 1.15, the flag FLG weak is switched ON; and when the flag FLG weak is ON and the K hV1 decreases to 1.10, the flag FLG weak is switched OFF.
- the weak field control unit 31 when the weak field control flag FLG weak is OFF and the low range component K hV1_fil2 of the motor voltage modulation rate reaches 1.10, the flag FLG weak is switched ON; and when the flag FLG weak is ON and the low range component K hV1_fil2 of the motor voltage modulation rate decreases to 1.05, the flag FLG weak is switched OFF.
- the configuration other than the above configuration of the controller 12 is the same as of the first embodiment (see FIG. 2 ).
- the weak field control unit 31 Based on the low range component K hV1_fil2 of the motor voltage modulation rate, which component is obtained after the motor voltage modulation rate K hV1 is subjected beforehand to low-pass filter processing, the weak field control unit 31 according to this embodiment sets the ON/OFF state of the weak field control flag FLG weak . Accordingly, the flag FLG weak is switched less frequently.
- the flag FLG weak when the low range component K hV1_fil2 of the motor voltage modulation rate reaches 1.10, the flag FLG weak is switched ON as described above. Thus, before the motor voltage modulation rate K hV1 reaches 1.15, the flag FLG weak can be actually switched ON. This can prevent the occurrence of the state where the weak field control voltage-manipulating variable cannot be adjusted while the output voltage of the inverter device 3 is saturated.
- the controller (12) includes: the low-pass filter (54) into which a value (K hV1 ) changed in response to a change in the DC voltage (V dc ) is input; and the weak field control unit (31) configured to determine, based on the output signal from the low-pass filter (54), whether or not the weak field control is executed.
- the weak field control unit (31) configured to determine, based on the output signal from the low-pass filter (54), whether or not the weak field control is executed.
- the configuration of this embodiment is the same as of the first embodiment ( FIGS. 1 and 2 ). However, as a control program executed in the weak field change-suppressing control unit 32, used is one illustrated in FIG. 17 instead of the program according to the first embodiment ( FIG. 6 ).
- Step S142 of FIG. 17 the low range component K hV1_fil of the motor voltage modulation rate, which component is obtained after the K hV1 is subjected to low-pass filter processing, is calculated.
- Step S144 it is determined whether or not the weak field control flag FLG weak is OFF. If Step S144 is judged as "YES”, the process goes to Step S148.
- the maximum max (K hV1 ) of the motor voltage modulation rate K hV1 during a past predetermined period e.g., 20 milliseconds
- Step S148 If Step S148 is judged as "YES”, the process goes to Step S150 and the d-axis current command value I d * is calculated based on the above [Expression 10]. Then, the process of this routine is ended. By contrast, if Step S148 is judged as "NO”, the process goes to Step S152 and the d-axis current command value I d * is set to 0. Then, the process of this routine is ended.
- Step S146 it is determined whether or not the minimum min (K hV1 ) of the motor voltage modulation rate K hV1 during a past predetermined period (e.g., 20 milliseconds) is 1.00 or more and 1.10 or less. If Step S146 is judged as "YES”, the process goes to Step S150 and the d-axis current command value I d * is calculated based on the above [Expression 10]. Then, the process of this routine is ended. By contrast, if Step S146 is judged as "NO”, the process goes to Step S152 and the d-axis current command value I d * is set to 0. Then, the process of this routine is ended.
- the d-axis current command value (I d *) can be controlled based on the minimum min (K hV1 ) and the maximum max (K hV1 ) of the motor voltage modulation rate K hV1 during the past predetermined period.
- This like the first embodiment, enables the motor 4 to be driven stably.
- the configuration of this embodiment is substantially the same as of the first embodiment ( FIGS. 1 and 2 ). However, as a control program executed in the weak field change-suppressing control unit 32, used is one illustrated in FIG. 18 instead of the program according to the first embodiment ( FIG. 6 ).
- Step S162 of FIG. 18 the low range component K hV1_fil of the motor voltage modulation rate, which component is obtained after the K hV1 is subjected to low-pass filter processing, is calculated.
- Step S164 it is determined whether or not the low range component K hV1_fil of the motor voltage modulation rate is 1.05 or more and 1.20 or less. If this step is judged as "YES”, the process goes to Step S166 and the weak field change-suppressing control unit 32 uses the algorithm (its details are described below) shown in FIG. 19 to calculate the d-axis current command value I d *.
- Step S167 it is determined whether or not the d-axis current command value I d * calculated is a predetermined value I d_SET2 (its details are described below) or more. If this step is judged as "YES”, the process of this routine is ended and the d-axis current command value I d * calculated in the previous Step S166 is used. Alternatively, if either Step S164 or Step S167 is judged as "NO”, the process goes to Step S168 and the weak field change-suppressing control unit 32 sets the d-axis current command value I d * to 0.
- FIG. 19 is a block diagram illustrating a main section of the weak field change-suppressing control unit 32 according to this embodiment.
- the low-pass filter (LPF) 40 is used to subject the motor voltage modulation rate K hV1 to low-pass filter processing so as to output the low range component K hV1_fil of the motor voltage modulation rate.
- the subtracter 42 subtracts the low range component K hV1_fil of the motor voltage modulation rate from a target value 1.20.
- the integral control unit 44 executes proportional integral control using a value after this subtraction.
- the limiter processing unit 46 executes limiter processing such that the lower limit of the output signal from the integral control unit 44 is set to 0. Then, the resulting value is output as the d-axis current command value I d *.
- the integral control unit 44 controls the d-axis current command value I d * so as to make the low range component K hV1_fil of the motor voltage modulation rate closer to the target value 1.20. This enables the low range component K hV1_fil of the motor voltage modulation rate to be kept almost constant (at a value at or near the target value 1.20) regardless of the characteristics of the motor 4.
- FIG. 20 is a graph showing the relationship among the d-axis current command value I d *, the inverter frequency command value ⁇ 1 *, and the motor voltage modulation rate K hV1 according to this embodiment.
- the q-axis current command value I q * is kept constant; and while the inverter frequency command value ⁇ 1 * is increased, indicated are the d-axis current command value I d *, the maximum/minimum of the motor voltage modulation rate K hV1 , and the low range component K hV1_fil of the motor voltage modulation rate.
- the inverter frequency command value ⁇ 1 * increases, the low range component K hV1_fil of the motor voltage modulation rate becomes larger.
- the above Step S164 and S168 are executed and the d-axis current command value I d * is set to 0.
- Step S164 is then judged as "YES” and Step S166 is executed. Accordingly, the algorithm of FIG. 19 is used to calculate the d-axis current command value I d * such that the low range component K hV1_fil of the motor voltage modulation rate is about 1.20. As long as the calculated I d * is the predetermined value I d_SET2 or less, this calculated I d * is supplied, as it is, to the current control unit 25 (see FIG. 16 ). Note that the predetermined value I d_SET2 is a value at which various defects may occur after the I d * is increased to that value or more, and should be adjusted in accordance with the characteristics of the motor 4.
- the K hV1_fil when the low range component K hV1_fil of the motor voltage modulation rate is 1.05, the K hV1_fil abruptly rises and reaches 1.20.
- the frequency ⁇ P61 is set to the inverter frequency command value ⁇ 1 * where the K hV1_fil abruptly rises.
- the case where the d-axis current command value I d * is set to a value other than 0 means the case where "a magnetic flux that weakens the magnetic flux of the permanent magnets of the motor 4 is generated".
- the d-axis current command value I d * is set to be a negative value.
- the d-axis current command value I d * is set to be a positive value as shown in FIG. 20 .
- the weak field control unit 31 switches the FLG weak from OFF to ON; and when the K hV1 decreases to 1.10, the weak field control unit 31 switches the FLG weak from ON to OFF.
- the weak field control flag FLG weak is kept ON, so that the FLG weak is switched less frequently.
- Step S164 (see FIG. 18 ) is judged as "NO". Then, at Step S168, the I d * is set to 0.
- the frequency ⁇ P62 is referred to as the inverter frequency command value ⁇ 1 * at which the low range component K hV1_fil of the motor voltage modulation rate starts rising again and is beyond 1.20.
- the d-axis current command value I d * is calculated based on the algorithm of FIG. 19 .
- the d-axis current command unit (32) controls, when the output voltage is lower than the saturation level, the d-axis current command value (I d *) such that a magnetic flux that strengthens a magnetic flux generated by the permanent magnets is generated in the windings.
- This like the first embodiment, enables the motor 4 to be driven stably.
- FIG. 21 is a schematic view of the air conditioner W according to the seventh embodiment.
- the air conditioner W includes an indoor unit U1, an outdoor unit U2, a pipe k connecting therebetween, and a remote controller Re.
- the air conditioner W is an apparatus through which a heat-transfer medium circulates using a well-known heat pump cycle so as to execute air conditioning (e.g., cooling operation, heating operation, dehumidification operation).
- the remote controller Re is to send or receive various predetermined signals (e.g., to give an operation/stop command, to change a set temperature, to set a timer, to change an operation mode) to or from the indoor unit U1.
- the outdoor unit U2 includes an electronics case 80 that houses various electronics and a compressor 82.
- the electronics case 80 includes the converter circuit 2 (see FIG. 1 ) and the inverter device 3 (see FIG. 1 ) according to any one of the above first to sixth embodiments.
- the inside of the compressor 82 is provided with the above-described motor 4.
- the flag FLG weak can be prevented from being switched frequently, which allows for continuously stable operation.
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Abstract
Description
- The present invention relates to a power conversion device and an air conditioner.
- The Abstract of the following
Patent Literature 1, which relates to a technology of weak field control for a permanent magnet synchronous motor, recites "To smoothly switch between vector control featuring a current command calculation unit and voltage phase operation type weak field control, and to improve the efficiency in switching" and "The problem is solved by any one of followings or combination of them. 1. A step is provided for reducing a voltage phase acquired from intermediate voltage command values Vdc* and Vqc* when switching from normal control to voltage phase operation type weak field control. 2. A value acquired by averaging d-axis current detection values is taken as a first d-axis current command value to be input in a d-axis current command calculation unit when returning to the normal control from the voltage phase operation type weak field control. 3. The gain of the d-axis current command calculation unit is switched when returning to the normal control from the voltage phase operation type weak field control. 4. A motor constant (resistance, inductance, power generation constant) identification calculation unit is provided in addition to the normal control and voltage phase operation type weak field control". - Patent Literature 1: Japanese Patent Application Publication No.
2010-142030 - Here, it is assumed that AC voltage from, for instance, a commercial power source is converted to DC voltage by using a converter circuit; the DC voltage is further converted to AC voltage with each given frequency by an inverter device; and the AC voltage is used to drive a permanent magnet synchronous motor (hereinafter, referred to as a "motor"). When the AC voltage from a commercial power source has distortions and/or when a cheap converter circuit is used, the DC voltage output from the converter circuit has convoluted ripple components. The ripple components of the DC voltage may cause an ON/OFF state of weak field control to be switched frequently. This switching induces distortion in the output voltage or current of the inverter device, thereby making the motor unstable. This may cause problems such as a stoppage due to overcurrent, malfunctions, a rapid change in the rotation speed.
- The present invention has been made in view of the above-mentioned situations. The purpose of the present invention is to provide a power conversion device allowing for stable operation of motors and an air conditioner therewith.
- An aspect of the present invention provides a power conversion device comprising:
- an inverter which converts, in order to drive a motor equipped with a stator having windings and a rotor having permanent magnets, supplied DC voltage to an AC output voltage and supplies the AC output voltage to the windings, wherein, a saturation level at which the output voltage is saturated changes in accordance with the DC voltage; and
- a controller which, when the output voltage is lower than the saturation level, increases an output current of the inverter to generate in the windings a magnetic flux in such a direction as to weaken or strengthen a magnetic flux generated by the permanent magnets.
- The present invention enables motors to be driven stably.
-
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FIG. 1 is a block diagram showing a motor drive system according to a first embodiment of the present invention. -
FIG. 2 is a block diagram illustrating a controller according to the first embodiment. -
FIG. 3 is a waveform diagram showing a pre-modulation U-phase voltage modulation rate, a triangular-wave modulating signal, and a post-modulation U-phase voltage modulation rate according to the first embodiment. -
FIG. 4 is waveform diagrams illustrating PWM signals and a carrier signal according to the first embodiment. -
FIG. 5 is a diagram showing a phase relation among d-axis and q-axis voltage command values at the time of weak field control and a voltage command wave high point according to the first embodiment. -
FIG. 6 is a flow chart of a control program executed in a weak field change-suppressing control unit according to the first embodiment. -
FIG. 7 is a graph showing the relationship among a d-axis current command value, an inverter frequency command value, and a motor voltage modulation rate according to the first embodiment. -
FIG. 8 is a graph showing another relationship among the d-axis current command value, the inverter frequency command value, and the motor voltage modulation rate according to the first embodiment. -
FIG. 9 is a flow chart of a control program executed in a weak field change-suppressing control unit according to a second embodiment. -
FIG. 10 is a block diagram illustrating a main section of the weak field change-suppressing control unit according to the second embodiment. -
FIG. 11 is a graph showing the relationship among a d-axis current command value, an inverter frequency command value, and a motor voltage modulation rate according to the second embodiment. -
FIG. 12 is a graph showing another relationship among the d-axis current command value, the inverter frequency command value, and the motor voltage modulation rate according to the second embodiment. -
FIG. 13 is a block diagram illustrating a main section of a controller according to a third embodiment. -
FIG. 14 is a flow chart of a control program executed in a weak field change-suppressing control unit according to the third embodiment. -
FIG. 15 is a graph showing another relationship among the d-axis current command value, the inverter frequency command value, and the motor voltage modulation rate according to the third embodiment. -
FIG. 16 is a block diagram illustrating a controller according to a fourth embodiment. -
FIG. 17 is a flow chart of a control program executed in a weak field change-suppressing control unit according to a fifth embodiment. -
FIG. 18 is a flow chart of a control program executed in a weak field change-suppressing control unit according to a sixth embodiment. -
FIG. 19 is a block diagram illustrating a main section of the weak field change-suppressing control unit according to the sixth embodiment. -
FIG. 20 is a graph showing another relationship among the d-axis current command value, the inverter frequency command value, and the motor voltage modulation rate according to the sixth embodiment. -
FIG. 21 is a schematic view of an air conditioner according to a seventh embodiment. - [First Embodiment] The following describes, in detail, a motor drive system S1 according to the first embodiment of the present invention.
-
FIG. 1 is a block diagram showing the motor drive system S1 according to the first embodiment of the present invention. InFIG. 1 , the motor drive system S1 includes: aconverter circuit 2 in which AC voltage from anAC voltage source 1 is converted to DC voltage; an inverter device 3 (power conversion device); and a permanent magnet synchronous motor 4 (hereinafter, referred to as a motor 4). Themotor 4 is provided with a rotor having permanent magnets embedded (not shown) and a stator having windings (not shown). TheAC voltage source 1 supplies 3-phase AC voltage to theconverter circuit 2. - The
converter circuit 2 includes a 3-phase diode bridge 5, aDC reactor 6, and a smoothing capacitor 7. When 3-phase AC voltage is supplied from theAC voltage source 1 to the 3-phase diode bridge 5, the 3-phase diode bridge 5 outputs full-wave-rectified voltage. The 3-phase diode bridge 5 outputs the voltage on the P side and the N side. The P side is connected to theDC reactor 6. The smoothing capacitor 7 is connected to theDC reactor 6 output side and the 3-phase diode bridge 5 output N side. Then, theconverter circuit 2 outputs, as a DC voltage, an inter-terminal voltage of the smoothing capacitor 7. - The DC voltage output from the
converter circuit 2 is input into theinverter device 3. Theinverter device 3 includes: a DC voltage detection circuit 8; an intelligent power module (IPM) 9 with an inverter function; a U-phase motorcurrent detection circuit 10; a V-phase motorcurrent detection circuit 11; acontroller 12; and agate drive circuit 13. - The DC voltage supplied from the
converter circuit 2 is input into the IPM 9 (inverter). TheIPM 9 includes 6 IGBTs and free-wheeling diodes (FWD) connected in parallel to the respective IGBTs (both are not numbered). Then, theIPM 9 converts the DC voltage to 3-phase AC voltage by switching each IGBT ON/OFF through using agate drive signal 18 supplied from thegate drive circuit 13. This 3-phase AC voltage is an output of theinverter device 3. Meanwhile, the DC voltage detection circuit 8 measures the DC voltage input into theinverter device 3 and sends, as a DCvoltage detection signal 14, the measured results to thecontroller 12. - The 3-phase AC voltage output from the
inverter device 3 is applied to windings of themotor 4. In addition, a U-phase motorcurrent detection circuit 10 and a V-phase motorcurrent detection circuit 11 are disposed partway through paths of a U-phase current and a V-phase current, respectively, of 3-phase current flowing through themotor 4. Thesecurrent detection circuits controller 12, a U-phase motorcurrent detection signal 15 and a V-phase motorcurrent detection signal 16, respectively. Based on the DCvoltage detection signal 14, the U-phase motorcurrent detection signal 15, and the V-phase motorcurrent detection signal 16, thecontroller 12 calculates a DUTY ratio so as to switch ON/OFF each IGBT in theIPM 9 and outputs aPWM signal 17 with the DUTY ratio. ThePWM signal 17 is converted to agate drive signal 18 having an enough voltage to switch ON/OFF each IGBT in thegate drive circuit 13. - The
controller 12 includes general computer hardware such as a CPU (central processing unit), a RAM (random access memory), and a ROM (read only memory). The ROM stores, for example, a control program executed by the CPU and various data. -
FIG. 2 is a block diagram showing an algorithm of thecontroller 12 and illustrates functional blocks implemented by, for example, the control program. - In
FIG. 2 , the U-phase motorcurrent detection signal 15 and the V-phase motorcurrent detection signal 16 are input into an A/D converter 19. Then, the A/D converter 19 outputs, as a U-phase current detection value Iu and a V-phase current detection value Iv, the resulting values as obtained by multiplying the U-phase motorcurrent detection signal 15 and the V-phase motorcurrent detection signal 16 by corresponding predetermined gains (referred to as current detection circuit gains). - A
dq converter 20 receives the U-phase current detection value Iu, the V-phase current detection value Iv, and a d-axis phase θdc (its details are described below). Then, thedq converter 20 outputs a d-axis current detection value Idc and a q-axis current detection value Iqc calculated based on the following [Expression 1]. - Here, a coordinate system is assumed that rotates at the electrical angle of the motor 4 (value obtained by multiplying a mechanical angle by the number of pole pairs of the motor 4). In this coordinate system, a d-axis is set to the direction of a magnetic flux generated by the permanent magnets, and a q-axis is set to an axis perpendicular to the d-axis. The coordinate system having the d-axis and the q-axis is called a "dq-axis coordinate system". The above-mentioned d-axis current detection value Idc and q-axis current detection value Iqc are values of the dq-axis coordinate system.
- Meanwhile, an axis error calculator 21 receives the d-axis current detection value Idc, the q-axis current detection value Iqc, and an inverter frequency ω1. Then, the axis error calculator 21 calculates and outputs an axis error Δθc based on the following [Expression 2]. Note that in [Expression 2], Vd* is a d-axis voltage command value; Vq* is a q-axis voltage command value; R is resistance of the windings of the motor; Ld is motor d-axis inductance; and Lq is motor q-axis inductance.
- A
PLL control unit 22 uses the axis error Δθc as an input and executes proportional integral control to calculate the inverter frequency ω1. A d-axisphase updating unit 23 adds, to the previous output value (before 1 calculation cycle) of a d-axis phase θdc, a value Δθdc obtained by dividing the inverter frequency ω1 by that at the previous calculation cycle. Then, the d-axisphase updating unit 23 outputs the added value as a current value for the d-axis phase θdc. A speed control unit 24 (q-axis current command unit) calculates a deviation Δω (not shown) between an inverter frequency command value ω1* (frequency command value) and the inverter frequency ω1, and executes proportional integral control based on the deviation Δω to calculate a q-axis current command value Iq*. - A
current control unit 25 calculates a deviation ΔIq (not shown) between the q-axis current command value Iq* and the q-axis current detection value Iqc, and executes proportional integral control using the deviation ΔIq as an input to calculate a q-axis current command correction amount (not shown). In addition, thecurrent control unit 25 outputs, as a second q-axis current command value Iq**, a value obtained by adding the q-axis current command correction amount to the q-axis current command value Iq*. Further thecurrent control unit 25 executes proportional integral control using, as an input, a deviation ΔId (not shown) between the d-axis current command value Id* and the d-axis current detection value Idc, and then outputs the resulting value as a second d-axis current command value Id**. - A VdVq calculator 26 receives the inverter frequency command value ω1*, the second q-axis current command value Iq**, and the second d-axis current command value Id**, and calculates a d-axis voltage command value Vd* and a q-axis voltage command value Vq* by using the following [Expression 3]. Note that in [Expression 3], Ke is an induced voltage constant of the
motor 4. -
-
- Further, the
AVR calculator 27 calculates a DC voltage detection value Vdc, which is obtained by multiplying the DCvoltage detection signal 14 by a predetermined gain (referred to as a DC voltage detection circuit gain), and then calculates a motor voltage modulation rate KhV1 based on [Expression 6]. -
- Meanwhile, a
dq inverter unit 28 receives the d-axis voltage modulation rate KhVd, the q-axis voltage modulation rate KhVq, and the d-axis phase θdc, and outputs a U-phase voltage modulation rate Khvu, a V-phase voltage modulation rate KhVv, and a W-phase voltage modulation rate KhVw based on [Expression 8]. - Here, described is the meaning of "weak field control" used in this embodiment and the below-described additional embodiments. As used in this embodiment and the additional embodiments, the "weak field control" refers to the feature of controlling phases of the d-axis and q-axis voltage modulation rates KhVd and KhVq based on [Expression 7] and then generating, in the windings of the
motor 4, a magnetic flux that weakens a magnetic flux generated by the permanent magnets. As described below, even if the weak field control voltage-manipulating variable is 0, the magnetic flux that weakens the magnetic flux generated by the permanent magnets may be induced by controlling the d-axis current command value Id*. This operation may be similar to the weak field control, but is not called the "weak field control" in this embodiment and the additional embodiments. - In addition, the
modulation processing unit 29 modulates the U-, V-, and W-phase voltage modulation rates Khvu, KhVv, and Khvw by using a triangular wave-like modulating signal MD, and outputs post-modulation U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and KhVw'. Specifically, the post-modulation U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and Khvw' are expressed in [Expression 9]. -
FIG. 3 is a waveform diagram showing a pre-modulation U-phase voltage modulation rate KhVu, a modulating signal MD, and a post-modulation U-phase voltage modulation rate KhVu'. Note that a corresponding V-phase signal is delayed 120 degrees from the U-phase signal and a corresponding W-phase signal is delayed 240 degrees from the U-phase signal (not shown). - After the above-mentioned modulation processing is executed in the
modulation processing unit 29, the utilization rate of the DC voltage detection value Vdc improves. When compared with the case of subjecting themotor 4 to sine wave drive, the output voltage of the inverter device is increased by maximum 15%. In addition, themodulation processing unit 29 executes upper and lower limit processing. Specifically, the upper limit and the lower limit of the output value are restricted to 1 and -1, respectively. - Back to
FIG. 2 . APWM signal converter 30 compares how large or small the carrier signal CR is relative to the U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and Khvw', and then outputs aPWM signal 17. Here, thePWM signal 17 includes 6 signals: a U-phase P-side PWM signal, a U-phase N-side PWM signal, a V-phase P-side PWM signal, a V-phase N-side PWM signal, a W-phase P-side PWM signal, and a W-phase N-side PWM signal. -
FIG. 4 is waveform diagrams illustrating the PWM signals and a carrier signal CR. As shown, the carrier signal CR is a fixed-cycle triangular wave. Meanwhile, the P-side PWM signal and the N-side PWM signal of each phase are signals where the ON/OFF state is inverted. - When the output values of the
modulation processing unit 29, namely the U-, V-, and W-phase voltage modulation rates Khvu', KhVv', and Khvw', reach the upper limit (1) or the lower limit (-1), the output voltage of theinverter device 3 may be saturated, causing the motor to malfunction. This may stop themotor 4. In order to prevent themotor 4 from stopping in this way, the weakfield control unit 31 inFIG. 2 executes, when the motor voltage modulation rate KhV1 reaches 1.15, the weak field control. Specifically, the weakfield control unit 31 calculates a deviation ΔIq between the q-axis current command value Iq* and the q-axis current detection value Iqc, performs integral control using the deviation ΔIq as an input, and calculates a weak field control voltage-manipulating variable δθweak. - Further, when the motor voltage modulation rate KhV1 reaches 1.15, the weak
field control unit 31 switches a weak field control flag FLGweak from OFF to ON. The flag FLGweak is a flag that designates the ON/OFF state of the weak field control. When the weak field control flag FLGweak is ON, thecurrent control unit 25 terminates the proportional integral control using the deviation ΔIq (= Iq* - Iqc) and the deviation ΔId (= Id* - Idc). At this time, the integral term of the proportional integral control is not reset and the value before the termination of the proportional integral control is held. - Meanwhile, when the flag FLGweak is ON, the weak
field control unit 31, instead of thecurrent control unit 25, is used to correct the deviation ΔIq between the q-axis current command value Iq* and the q-axis current detection value Iqc by using feedback control. Note that the condition where the motor voltage modulation rate KhV1 reaches 1.15 means that the output voltage of theinverter device 3 gets saturated. This is the same as the condition where the output value (e.g., the U-phase voltage modulation rate KhVu' shown inFIG. 3 ) of themodulation processing unit 29 reaches the upper limit (1) or the lower limit (-1). The above-described KhV1 = 1.15 is the upper limit when themotor 4 is subject to sine wave drive (when a sine wave-like current flows through the motor 4). If themotor 4 is not subject to sine wave drive, the upper limit may be further elevated. -
FIG. 5 is a diagram showing a phase relation, in the dq-axis coordinate system, among a d-axis voltage command value Vd* and a q-axis voltage command value Vq* at the time of weak field control and a voltage command wave high point V1. As shown in [Expression 5], V1 is a synthetic vector of the Vd* and Vq*. Provided that in the weak field area, the phase of voltage applied to themotor 4 is a phase obtained by adding to the phase of Vi, namely the motor voltage phase δθ. In addition, when the FLGweak is ON and the KhV1 is lowered to 1.10, the weakfield control unit 31 switches the FLGweak to OFF. At this time, the integral term of the proportional integral control of the weakfield control unit 31 is cleared to 0. When the FLGweak is switched OFF, thecurrent control unit 25 resumes operation of the proportional integral control. - In this way, depending on the ON/OFF state of the flag FLGweak, the proportional integral control using the deviations ΔId and ΔIq in the
current control unit 25 is switched between stop and execution states. Because of this, if the ON/OFF state of the flag FLGweak is frequently switched, thecurrent control unit 25 is unstably operated. Here, in this embodiment, the flag FLGweak is switched less frequently so as to stably operate thecontroller 12. - Next, described is how to operate the weak field change-suppressing control unit 32 (d-axis current command unit) shown in
FIG. 2 . For instance, when AC voltage supplied from theAC voltage source 1 has distortion and/or when the electrostatic capacity of the smoothing capacitor 7 is small, the DC voltage output from theconverter circuit 2 may have convoluted ripple components. The ripple components are transferred, via the DCvoltage detection signal 14, to KhV1. As described above, when the KhV1 reaches 1.15, the weakfield control unit 31 switches the FLGweak from OFF to ON; and when the KhV1 decreases to 1.10, the weakfield control unit 31 switches the FLGweak from ON to OFF. Due to this, the FLGweak is switched frequently when the ripple components of the KhV1 are 0.05 or more. - To suppress this unstable operation, the weak field change-suppressing
control unit 32 adjusts the d-axis current command value Id* so as to prevent the KhV1 from fluctuating in a range from less than 1.10 to more than 1.15. -
FIG. 6 is a flow chart of a control program executed every given time in the weak field change-suppressingcontrol unit 32. - When the process goes to Step S102 of
FIG. 6 , the low range component KhV1_fil of the motor voltage modulation rate, which component is obtained after the KhV1 is subjected to low-pass filter processing, is calculated. - Next, when the process goes to Step S104, it is determined whether or not the weak field control flag FLGweak is OFF. If the flag FLGweak is OFF, this step is judged as "YES". Then, the process goes to Step S108. At Step S108, it is determined whether or not the low range component KhV1_fil of the motor voltage modulation rate is 1.05 or more and 1.10 or less. If this step is judged as "YES", the process goes to Step S110. At Step S110, the d-axis current command value Id* is calculated based on [Expression 10]. Provided that K of [Expression 10] is a proportional gain.
- Meanwhile, if the FLGweak is OFF ("YES" at Step S104) and the KhV1_fil is less than 1.05 or more than 1.10, the process goes to Step S112. Here, the Id* is set to 0.
-
FIG. 7 is a graph showing the relationship among the d-axis current command value Id*, the inverter frequency command value ω1*, and the motor voltage modulation rate KhV1. - Specifically, in
FIG. 7 , the q-axis current command value Iq* is kept constant; the abscissa represents the inverter frequency command value ω1*, which is increased; and the ordinate represents the d-axis current command value Id*, the maximum/minimum of the motor voltage modulation rate KhV1, and the low range component KhV1_fil of the motor voltage modulation rate. As the inverter frequency command value ω1* increases, the low range component KhV1_fil of the motor voltage modulation rate becomes larger. When the KhV1_fil is less than 1.05, Step S112 ofFIG. 6 is executed and the d-axis current command value Id* is set to 0. - As soon as the inverter frequency command value ω1* reaches the frequency ωP1, the KhV1_fil is 1.05 or more. Then, Step S110 of
FIG. 6 is executed, so that the Id* starts decreasing (the absolute value starts increasing). While the absolute value of the Id* is increased, the slope of the KhV1_fil gets less steep. As soon as the inverter frequency command value ω1* reaches the frequency ωP2, the KhV1_fil is 1.10 or more. Then, Step S112 ofFIG. 6 is re-executed. At this step, the Id* is set to 0, so that the KhV1_fil abruptly rises as shown inFIG. 7 . - In this way, after the KhV1_fil abruptly rises, the maximum of the KhV1 is 1.15 or more and the minimum of the KhV1 is 1.10 or more as shown in
FIG. 7 where ω1* > ωP2. As described above, when the KhV1 reaches 1.15, the weakfield control unit 31 switches the FLGweak from OFF to ON; and when the KhV1 decreases to 1.10, the weakfield control unit 31 switches the FLGweak from ON to OFF. Hence, inFIG. 7 where ω1* > ωP2, the FLGweak is switched less frequently. - If the weak field control flag FLGweak is switched ON, Step S104 is judged as "NO" when the control program (
FIG. 6 ) is next implemented. Then, the process goes to Step S106. Here, whether or not the low range component KhV1_fil of the motor voltage modulation rate is 1.05 or more and 1.15 or less is determined. InFIG. 7 where the ω1* is frequency ωP2 or more, the KhV1_fil exceeds 1.15, so that this step is judged as "NO". Then, the process goes to Step S112. Due to this, the d-axis current command value Id* is kept constant at 0. - If the ω1* decreases from this state (the flag FLGweak is ON) and the low range component KhV1_fil of the motor voltage modulation rate is 1.05 or more and 1.15 or less, Step S106 is judged as "YES". Here, at Step S110, the d-axis current command value Id* is calculated based on [Expression 10]. Meanwhile, if the FLGweak is ON and the KhV1_fil is less than 1.05, the Id* is set to 0 at Step S110.
-
FIG. 8 is a graph showing another relationship among the d-axis current command value Id*, the inverter frequency command value ω1*, and the motor voltage modulation rate KhV1. - Specifically, in
FIG. 8 , the q-axis current command value Iq* is kept constant; the abscissa represents the inverter frequency command value ω1*, which is decreased; and the ordinate represents the d-axis current command value Id*, the maximum/minimum of the motor voltage modulation rate KhV1, and the low range component KhV1_fil of the motor voltage modulation rate. - As the ω1* decreases, the KhV1_fil also decreases. When the KhV1_fil becomes 1.15 or less at the frequency ωP4, the Id* decreases stepwise (the absolute value increases) and the KhV1 also decreases stepwise. This allows the maximum of the KhV1 to be less than 1.15 and the minimum of the KhV1 to be less than 1.10, so that the FLGweak is switched less frequently.
- As described above, this embodiment includes: an inverter (9) which converts supplied DC voltage (Vdc) to an AC output voltage and supplies the AC output voltage to windings, and which, in accordance with the DC voltage (Vdc), changes a saturation level at which the output voltage is saturated, in order to drive a motor (4) equipped with a stator having the windings and a rotor having permanent magnets; and a controller (12) which, when the output voltage is lower than the saturation level, increases an output current of the inverter such that a magnetic flux that weakens or strengthens a magnetic flux generated by the permanent magnets is generated in the windings.
- In addition, the controller (12) includes, when in a coordinate system that rotates at a rotation speed of the electrical angle of the motor (4), a d-axis is set to the direction of a magnetic flux generated by the permanent magnets and a q-axis is set to an axis perpendicular to the d-axis, the q-axis current command unit (24) configured to output the q-axis current command value (Iq*), which is a command value for the q-axis component of the output voltage, based on the frequency command value (ω1*); and the d-axis current command unit (32) configured to output the d-axis current command value (Id*), which is a command value for the d-axis component of the output current, based on the frequency command value (ω1*), wherein the d-axis current command unit (32) controls, when the output voltage is lower than the saturation level, the d-axis current command value (Id*) such that a magnetic flux that weakens a magnetic flux generated by the permanent magnets is generated in the windings.
- That is, based on the low range component KhV1_fil of the motor voltage modulation rate, Steps S110 and S112 set the d-axis current command value Id*. This can prevent the flag FLGweak from being switched frequently, allowing for stable operation of the
motor 4. - [Second Embodiment] The following describes, in detail, a motor drive system according to the second embodiment of the present invention. Note that in the description below, elements corresponding to the respective elements of
FIGS. 1 to 8 have the same reference numerals so as to avoid redundancy. - The weak field change-suppressing
control unit 32 according to the above first embodiment executes the proportional control in [Expression 10]. The proportional gain K of this proportional control is preferably adjusted in accordance with characteristics of themotor 4. Specifically, when the proportional gain K is too large, the d-axis current is too small (the absolute value is too large), causing a problem of increasing a loss in themotor 4 or theinverter device 3. By contrast, when the proportional gain K is too small, a problem occurs where the weak field control flag FLGweak is switched frequently. Here, this embodiment is to mitigate complexities of changing the proportional gain K in accordance with the characteristics of themotor 4. - The configuration of this embodiment is the same as of the first embodiment (
FIGS. 1 and2 ). However, as a control program executed in the weak field change-suppressingcontrol unit 32, used is one illustrated inFIG. 9 instead of the program according to the first embodiment (FIG. 6 ). - When the process goes to Step S122 of
FIG. 9 , the low range component KhV1_fil of the motor voltage modulation rate, which component is obtained after the motor voltage modulation rate KhV1 is subjected to low-pass filter processing, is calculated. Next, when the process goes to Step S124, whether or not the KhV1_fil is 1.05 or more and 1.15 or less is determined. If this step is judged as "YES", the process goes to Step S126 and the d-axis current command value Id* is then calculated. -
FIG. 10 is a block diagram illustrating a main section of the weak field change-suppressingcontrol unit 32 according to this embodiment. That is,FIG. 10 depicts, as blocks, content of the d-axis current command value Id* calculation processing executed in the above Step S126. - In
FIG. 10 , a low-pass filter (LPF) 40 is used to subject the motor voltage modulation rate KhV1 to low-pass filter processing so as to output the low range component KhV1_fil of the motor voltage modulation rate. Thesubtracter 42 subtracts the low range component KhV1_fil of the motor voltage modulation rate from a target value 1.05. Anintegral control unit 44 executes proportional integral control using a value after this subtraction. Alimiter processing unit 46 executes limiter processing such that the upper limit of the output signal from theintegral control unit 44 is set to 0. Then, the resulting value is output as the d-axis current command value Id*. - Back to
FIG. 9 . When the process goes to Step S127, it is determined whether or not the d-axis current command value Id* is a predetermined value Id_SET or more. If this step is judged as "YES", the process of this routine is ended. Here, based on the d-axis current command value Id* calculated in Step S126, a d-axis current is controlled. In addition, if either Step S124 or S127 is judged as "NO", the process goes to Step S128 and the d-axis current command value Id* is set to 0. Then, the process of this routine is ended. - According to the processing of
FIG. 10 , theintegral control unit 44 controls the d-axis current command value Id* so as to make the low range component KhV1_fil of the motor voltage modulation rate closer to the target value 1.05. This enables the low range component KhV1_fil of the motor voltage modulation rate to be kept almost constant (at a value at or near the target value 1.05) regardless of the characteristics of themotor 4. -
FIG. 11 is a graph showing the relationship among the d-axis current command value Id*, the inverter frequency command value ω1*, and the motor voltage modulation rate KhV1 according to this embodiment. - Specifically, in
FIG. 11 like the aboveFIG. 7 , the q-axis current command value Iq* is kept constant; and while the inverter frequency command value ω1* is increased, indicated are the d-axis current command value Id*, the maximum/minimum of the motor voltage modulation rate KhV1, and the low range component KhV1_fil of the motor voltage modulation rate. - In
FIG. 11 , as the inverter frequency command value ω1* increases, the low range component KhV1_fil of the motor voltage modulation rate becomes larger. When the KhV1_fil is less than 1.05, the above Step S128 (seeFIG. 6 ) is executed and the d-axis current command value Id* is set to 0. - Once the low range component KhV1_fil of the motor voltage modulation rate is 1.05, Step S124 (see
FIG. 6 ) is then judged as "YES". Subsequently, Step S126 is executed, so that even if the inverter frequency command value ω1* is then increased, the KhV1_fil stays at almost 1.05. The frequency ωP21 is set to the inverter frequency command value ω1* where the low range component KhV1_fil of the motor voltage modulation rate reaches 1.05. - While the low range component KhV1_fil of the motor voltage modulation rate is kept at the target value 1.05, the Id* decreases (the absolute value increases) as the ω1* increases. Because the absolute value of the Id* is increased, the KhV1_fil is kept constant. The condition where the low range component KhV1_fil of the motor voltage modulation rate is kept constant is the same as the condition where the output voltage of the
inverter device 3 is kept substantially constant. When the Id* becomes less than the predetermined value Id_SET, Step S128 ofFIG. 9 is re-executed and the d-axis current command value Id* is thus set to 0. Due to this, the KhV1_fil abruptly rises. The frequency ωP22 is set to the inverter frequency command value ω1* at the timing of the abrupt rise. - In this way, after the KhV1_fil abruptly rises, the maximum of the motor voltage modulation rate KhV1 exceeds 1.15 and the minimum exceeds 1.10 as shown in
FIG. 11 where ω1* > ωP22. As described above, when the KhV1 reaches 1.15, the weakfield control unit 31 switches the FLGweak from OFF to ON; and when the KhV1 decreases to 1.10, the weakfield control unit 31 switches the FLGweak from ON to OFF. Hence, inFIG. 11 where ω1* > ωP22, the weak field control flag FLGweak is kept ON, so that the FLGweak is switched less frequently. Here, the predetermined value Id_SET is a value at which various defects may occur after the Id* is decreased to that value or less, and should be adjusted in accordance with the characteristics of themotor 4. -
FIG. 12 is a graph showing another relationship among the d-axis current command value Id*, the inverter frequency command value ω1*, and the motor voltage modulation rate KhV1 according to this embodiment. - Specifically, in
FIG. 12 , the q-axis current command value Iq* is kept constant; and while the inverter frequency command value ω1* is decreased, indicated are the d-axis current command value Id*, the maximum/minimum of the motor voltage modulation rate KhV1, and the low range component KhV1_fil of the motor voltage modulation rate. - As the ω1* decreases from the depicted maximum, the KhV1_fil also decreases. When the KhV1_fil becomes 1.15 or less at the frequency ωP24, the Id* decreases stepwise (the absolute value increases) and the KhV1_fil also decreases stepwise to the target value 1.05. In the region where the frequency is less than ωP24, the maximum of the motor voltage modulation rate KhV1 is less than 1.15 and the minimum is less than 1.10. This permits the flag FLGweak to be switched OFF by the weak
field control unit 31. This OFF state stays continuously. Because of the above, The FLGweak is switched less frequently. - As described above, according to this embodiment, the d-axis current command unit (32) controls the d-axis current command value (Id*) such that the output voltage is kept substantially constant while the frequency command value (ω1*) changes. More specifically, based on the low range component KhV1_fil of the motor voltage modulation rate, the d-axis current command value Id* is set in Steps S126 and S128. This, like the first embodiment, can prevent the flag FLGweak from being switched frequently. Besides, the d-axis current command value Id* can be set without using [Expression 10] (without using the proportional gain K). Hence, it is possible to mitigate complexities of setting the proportional gain K in accordance with the characteristics of the
motor 4. - [Third Embodiment] The following describes, in detail, a motor drive system according to the third embodiment of the present invention.
- In the weak field change-suppressing
control unit 32 according to the above second embodiment, the predetermined value Id_SET has been adjusted in accordance with the characteristics of themotor 4. In this embodiment, this adjustment is unnecessary, and it is possible to mitigate complexities of changing various parameters in accordance with the characteristics of themotor 4. - The configuration of this embodiment is similar to that of the first embodiment (
FIGS. 1 and2 ), but the algorithm of thecontroller 12 differs from that of the first embodiment (FIG. 2 ). -
FIG. 13 is a block diagram illustrating a main section of the algorithm of thecontroller 12 according to this embodiment. Note that in the description below, elements corresponding to the respective elements ofFIGS. 1 to 12 have the same reference numerals so as to avoid redundancy. The configuration of thecontroller 12 according to this embodiment is substantially the same as of the first embodiment (seeFIG. 2 ). However, acurrent control unit 33 shown inFIG. 13 is used as an alternative for thecurrent control unit 25 shown inFIG. 2 . In addition, as shown inFIG. 13 , thecontroller 12 according to this embodiment includes anadder 35, a VdVq controller 36, and anAVR calculator 37. - The
current control unit 33 includessubtracters integral control units adder 335. In thecurrent control unit 33, thesubtracter 331 subtracts a d-axis current detection value Idc from 0. Theintegral control unit 332 executes proportional integral control using a value (-Idc) after this subtraction, and the resulting value is output as a second d-axis current command value Id**. Provided that the proportionalintegral control unit 332 stops its operation when the low range component KhV1_fil of the motor voltage modulation rate is 1.05 or more. At this time, the integral term is not cleared to 0 and the value is held. - In addition, the
adder 35 adds the d-axis current command value Id* and the second d-axis current command value Id**. Based on the second q-axis current command value Iq**, the resulting value (Id* + Id**) added by theadder 35, and the inverter frequency command value ω1*, theVdVq calculator 26 calculates d-axis and q-axis voltage command values Vd* and Vq*. Specifically, instead of the "Id**" in the above [Expression 3], the "Id* + Id**" is used to give the d-axis and q-axis voltage command values Vd* and Vq*. - Meanwhile, based on the second d-axis current command value Id**, the second q-axis current command value Iq**, and the inverter frequency command value ω1*, the VdVq calculator 36 calculates a d-axis voltage-determining value Vd_SET and a q-axis voltage-determining value Vq_SET. Specifically, the d-axis and q-axis voltage command values Vd* and Vq* in [Expression 3] according to the above first embodiment correspond to the d-axis and q-axis voltage-determining values Vd_SET and Vq_SET according to this embodiment, respectively.
- Here, the
AVR calculator 27 calculates, like calculations using the above [Expression 4], [Expression 5], and [Expression 6], the motor voltage modulation rate KhV1. In addition, in the above [Expression 4], [Expression 5], and [Expression 6], the d-axis and q-axis voltage command values Vd* and Vq* are replaced by the d-axis and q-axis voltage-determining values Vd_SET and Vq_SET and the motor voltage modulation rate KhV1 is replaced by the motor voltage modulation rate-determining value KhV1_SET. Then, theAVR calculator 37 uses the resulting Expressions to calculate the motor voltage modulation rate-determining value KhV1_SET. - The motor voltage modulation rate KhV1 and the motor voltage modulation rate-determining vale KhV1_SET as so calculated are sent to the weak field change-suppressing
control unit 32. - If the low range component of the motor voltage modulation rate-determining value KhV1_SET is less than 1.15 and 1.05 or more, the weak field change-suppressing
control unit 32 according to this embodiment calculates the d-axis current command value Id* by using the algorithm shown inFIG. 10 . The following describes, in detail, processing of this weak field change-suppressingcontrol unit 32. -
FIG. 14 is a flow chart of a control program executed in the weak field change-suppressingcontrol unit 32 according to this embodiment instead of the first embodiment (FIG. 6 ). - When the process goes to Step S132 of
FIG. 14 , the low range component KhV1_fil of the motor voltage modulation rate, which component is obtained after the KhV1 is subjected to low-pass filter processing, is calculated. Next, when the process goes to Step S133, the low range component KhV1_SETfil of the motor voltage modulation rate-determining value, which component is obtained after the KhV1_SET is subjected to low-pass filter processing, is calculated. - Next, when the process goes to Step S134, whether or not the KhV1_SETfil is 1.05 or more and 1.15 or less is determined. If this step is judged as "YES", the process goes to Step S136 and the weak field change-suppressing
control unit 32 uses the algorithm shown inFIG. 10 to calculate the d-axis current command value Id*. If Step S134 is judged as "NO", the process goes to Step S138 and the weak field change-suppressingcontrol unit 32 sets the d-axis current command value Id* to 0. -
FIG. 15 is a graph showing another relationship among the d-axis current command value Id*, the inverter frequency command value ω1*, and the motor voltage modulation rate KhV1 according to this embodiment. - Specifically, in
FIG. 15 , the q-axis current command value Iq* is kept constant; and while the inverter frequency command value ω1* is increased, indicated are the d-axis current command value Id*, the maximum/minimum of the motor voltage modulation rate KhV1, the low range component KhV1_fil of the motor voltage modulation rate, and the low range component KhV1_SETfil of the motor voltage modulation rate-determining value. - In
FIG. 15 , as the inverter frequency command value ω1* increases, the low range component KhV1_fil of the motor voltage modulation rate becomes larger. After the KhV1_fil reaches 1.05, the KhV1_fil is, for a while, kept at almost the target value 1.05. Here, as the ω1* increases, the Id* decreases (the absolute value increases). The frequency ωP31 (first command value) is set to the inverter frequency command value ω1* where the KhV1_fil arrives at 1.05. Meanwhile, the low range component KhV1_SETfil of the motor voltage modulation rate-determining value is not affected by the d-axis current command value Id*. Thus, as shown in a dashed line ofFIG. 15 , the KhV1_SETfil continuously increases as the inverter frequency command value ω1* increases. - Next, when the KhV1_SETfil reaches 1.15, Step S138 of
FIG. 14 is executed and the d-axis current command value Id* is thus set to 0. Then, the low range component KhV1_fil of the motor voltage modulation rate abruptly rises. The frequency ωP32 (second command value) is set to the inverter frequency command value ω1* at the timing of the abrupt rise. - In this way, after the KhV1_fil abruptly rises, the maximum of the motor voltage modulation rate KhV1 exceeds 1.15 and the minimum exceeds 1.10 as shown in
FIG. 15 where ω1* > ωP32. As described above, when the KhV1 reaches 1.15, the weakfield control unit 31 switches the FLGweak from OFF to ON; and when the KhV1 decreases to 1.10, the weakfield control unit 31 switches the FLGweak from ON to OFF. Hence, inFIG. 15 where ω1* > ωP32, the weak field control flag FLGweak is kept ON, so that the FLGweak is switched less frequently. - As described above, according to this embodiment, the d-axis current command unit (32) sets, if the frequency command value (ω1*) is less than the first command value (ωP31), the d-axis current command value (Id*) to 0; increases, if the frequency command value (ω1*) is the first command value (ωP31) or more and less than the predetermined second command value (ωP32), the absolute value of the d-axis current command value (Id*) as the frequency command value (ω1*) becomes larger, so as to keep the output voltage substantially constant; and sets, if the frequency command value (ω1*) is the second command value (ωP32) or more, the d-axis current command value (Id*) to 0.
- More specifically, based on the low range component KhV1_SETfil of the motor voltage modulation rate-determining value, the d-axis current command value Id* is set in Steps S136 and S138. This, like the first embodiment, can prevent the flag FLGweak from being switched frequently. Further, the d-axis current command value Id* can be set without using the predetermined value Id_SET. Hence, it is possible to mitigate complexities of setting the predetermined value Id_SET in accordance with the characteristics of the
motor 4. - [Fourth Embodiment] The following describes, in detail, a motor drive system according to the fourth embodiment of the present invention.
- The configuration of this embodiment is similar to that of the first embodiment (
FIG. 1 ), but the algorithm of thecontroller 12 differs from that of the first embodiment. -
FIG. 16 is a block diagram showing the algorithm of thecontroller 12 and illustrates functional blocks implemented by, for example, the control program. Note that in the description below, elements corresponding to the respective elements ofFIGS. 1 to 15 have the same reference numerals so as to avoid redundancy. - In this embodiment, the
controller 12 has a low-pass filter 54. The low-pass filter 54 is used to subject the motor voltage modulation rate KhV1 to low-pass filter processing so as to output, to the weakfield control unit 31, the resulting value as the low range component KhV1_fil2 of the motor voltage modulation rate. The time constant of the low-pass filter 54 is sufficiently larger than the ripple frequency of the DC voltage detection value Vdc. - In the weak
field control unit 31 according to the above first embodiment, when the weak field control flag FLGweak is OFF and the motor voltage modulation rate KhV1 reaches 1.15, the flag FLGweak is switched ON; and when the flag FLGweak is ON and the KhV1 decreases to 1.10, the flag FLGweak is switched OFF. - By contrast, in the weak
field control unit 31 according to this embodiment, when the weak field control flag FLGweak is OFF and the low range component KhV1_fil2 of the motor voltage modulation rate reaches 1.10, the flag FLGweak is switched ON; and when the flag FLGweak is ON and the low range component KhV1_fil2 of the motor voltage modulation rate decreases to 1.05, the flag FLGweak is switched OFF. This point is a difference. The configuration other than the above configuration of thecontroller 12 is the same as of the first embodiment (seeFIG. 2 ). - Based on the low range component KhV1_fil2 of the motor voltage modulation rate, which component is obtained after the motor voltage modulation rate KhV1 is subjected beforehand to low-pass filter processing, the weak
field control unit 31 according to this embodiment sets the ON/OFF state of the weak field control flag FLGweak. Accordingly, the flag FLGweak is switched less frequently. - Provided that for instance, when the motor voltage modulation rate KhV1 abruptly rises, a response of the low range component KhV1_fil2 of the motor voltage modulation rate may be delayed. It is assumed that in this embodiment, the "1.15", which is identical to that of the first embodiment, is used as a threshold at which the flag FLGweak is set to ON. In this case, although the output voltage of the
inverter device 3 is saturated, the flag FLGweak is not switched ON. Consequently, the problem may occur where the weak field change-suppressingcontrol unit 32 cannot adjust the weak field control voltage-manipulating variable δθweak. - In this embodiment, when the low range component KhV1_fil2 of the motor voltage modulation rate reaches 1.10, the flag FLGweak is switched ON as described above. Thus, before the motor voltage modulation rate KhV1 reaches 1.15, the flag FLGweak can be actually switched ON. This can prevent the occurrence of the state where the weak field control voltage-manipulating variable cannot be adjusted while the output voltage of the
inverter device 3 is saturated. - As described above, the controller (12) according to this embodiment includes: the low-pass filter (54) into which a value (KhV1) changed in response to a change in the DC voltage (Vdc) is input; and the weak field control unit (31) configured to determine, based on the output signal from the low-pass filter (54), whether or not the weak field control is executed. This, like the first embodiment, enables the
motor 4 to be driven stably. - [Fifth Embodiment] The following describes, in detail, a motor drive system according to the fifth embodiment of the present invention. Note that in the description below, elements corresponding to the respective elements of
FIGS. 1 to 16 have the same reference numerals so as to avoid redundancy. - The configuration of this embodiment is the same as of the first embodiment (
FIGS. 1 and2 ). However, as a control program executed in the weak field change-suppressingcontrol unit 32, used is one illustrated inFIG. 17 instead of the program according to the first embodiment (FIG. 6 ). - When the process goes to Step S142 of
FIG. 17 , the low range component KhV1_fil of the motor voltage modulation rate, which component is obtained after the KhV1 is subjected to low-pass filter processing, is calculated. Next, when the process goes to Step S144, it is determined whether or not the weak field control flag FLGweak is OFF. If Step S144 is judged as "YES", the process goes to Step S148. Here, it is determined whether or not the maximum max (KhV1) of the motor voltage modulation rate KhV1 during a past predetermined period (e.g., 20 milliseconds) is 1.10 or more and 1.15 or less. - If Step S148 is judged as "YES", the process goes to Step S150 and the d-axis current command value Id* is calculated based on the above [Expression 10]. Then, the process of this routine is ended. By contrast, if Step S148 is judged as "NO", the process goes to Step S152 and the d-axis current command value Id* is set to 0. Then, the process of this routine is ended.
- If the flag FLGweak is OFF, the process goes to Step S146. Here, it is determined whether or not the minimum min (KhV1) of the motor voltage modulation rate KhV1 during a past predetermined period (e.g., 20 milliseconds) is 1.00 or more and 1.10 or less. If Step S146 is judged as "YES", the process goes to Step S150 and the d-axis current command value Id* is calculated based on the above [Expression 10]. Then, the process of this routine is ended. By contrast, if Step S146 is judged as "NO", the process goes to Step S152 and the d-axis current command value Id* is set to 0. Then, the process of this routine is ended.
- As described above, in this embodiment, the d-axis current command value (Id*) can be controlled based on the minimum min (KhV1) and the maximum max (KhV1) of the motor voltage modulation rate KhV1 during the past predetermined period.
- This, like the first embodiment, enables the
motor 4 to be driven stably. - [Sixth Embodiment] The following describes, in detail, a motor drive system according to the sixth embodiment of the present invention. Note that in the description below, elements corresponding to the respective elements of
FIGS. 1 to 17 have the same reference numerals so as to avoid redundancy. - The configuration of this embodiment is substantially the same as of the first embodiment (
FIGS. 1 and2 ). However, as a control program executed in the weak field change-suppressingcontrol unit 32, used is one illustrated inFIG. 18 instead of the program according to the first embodiment (FIG. 6 ). - When the process goes to Step S162 of
FIG. 18 , the low range component KhV1_fil of the motor voltage modulation rate, which component is obtained after the KhV1 is subjected to low-pass filter processing, is calculated. Next, when the process goes to Step S164, it is determined whether or not the low range component KhV1_fil of the motor voltage modulation rate is 1.05 or more and 1.20 or less. If this step is judged as "YES", the process goes to Step S166 and the weak field change-suppressingcontrol unit 32 uses the algorithm (its details are described below) shown inFIG. 19 to calculate the d-axis current command value Id*. - Next, when the process goes to Step S167, it is determined whether or not the d-axis current command value Id* calculated is a predetermined value Id_SET2 (its details are described below) or more. If this step is judged as "YES", the process of this routine is ended and the d-axis current command value Id* calculated in the previous Step S166 is used. Alternatively, if either Step S164 or Step S167 is judged as "NO", the process goes to Step S168 and the weak field change-suppressing
control unit 32 sets the d-axis current command value Id* to 0. -
FIG. 19 is a block diagram illustrating a main section of the weak field change-suppressingcontrol unit 32 according to this embodiment. - In
FIG. 19 , the low-pass filter (LPF) 40 is used to subject the motor voltage modulation rate KhV1 to low-pass filter processing so as to output the low range component KhV1_fil of the motor voltage modulation rate. Thesubtracter 42 subtracts the low range component KhV1_fil of the motor voltage modulation rate from a target value 1.20. Theintegral control unit 44 executes proportional integral control using a value after this subtraction. - The
limiter processing unit 46 executes limiter processing such that the lower limit of the output signal from theintegral control unit 44 is set to 0. Then, the resulting value is output as the d-axis current command value Id*. - According to the algorithm of
FIG. 19 , theintegral control unit 44 controls the d-axis current command value Id* so as to make the low range component KhV1_fil of the motor voltage modulation rate closer to the target value 1.20. This enables the low range component KhV1_fil of the motor voltage modulation rate to be kept almost constant (at a value at or near the target value 1.20) regardless of the characteristics of themotor 4. -
FIG. 20 is a graph showing the relationship among the d-axis current command value Id*, the inverter frequency command value ω1*, and the motor voltage modulation rate KhV1 according to this embodiment. - Specifically, in
FIG. 20 like the aboveFIGS. 7 and11 , the q-axis current command value Iq* is kept constant; and while the inverter frequency command value ω1* is increased, indicated are the d-axis current command value Id*, the maximum/minimum of the motor voltage modulation rate KhV1, and the low range component KhV1_fil of the motor voltage modulation rate. InFIG. 20 , as the inverter frequency command value ω1* increases, the low range component KhV1_fil of the motor voltage modulation rate becomes larger. When the KhV1_fil is less than 1.05, the above Step S164 and S168 (seeFIG. 18 ) are executed and the d-axis current command value Id* is set to 0. - Once the low range component KhV1_fil of the motor voltage modulation rate is 1.05, Step S164 is then judged as "YES" and Step S166 is executed. Accordingly, the algorithm of
FIG. 19 is used to calculate the d-axis current command value Id* such that the low range component KhV1_fil of the motor voltage modulation rate is about 1.20. As long as the calculated Id* is the predetermined value Id_SET2 or less, this calculated Id* is supplied, as it is, to the current control unit 25 (seeFIG. 16 ). Note that the predetermined value Id_SET2 is a value at which various defects may occur after the Id* is increased to that value or more, and should be adjusted in accordance with the characteristics of themotor 4. - In the instance of
FIG. 20 , when the low range component KhV1_fil of the motor voltage modulation rate is 1.05, the KhV1_fil abruptly rises and reaches 1.20. The frequency ωP61 is set to the inverter frequency command value ω1* where the KhV1_fil abruptly rises. At the frequency ωP61, the d-axis current command value Id* also steeply increases so as to achieve the KhV1_fil = 1.20. In the previous embodiments such as the first embodiment (seeFIG. 7 ), the case where the d-axis current command value Id* is set to a value other than 0 means the case where "a magnetic flux that weakens the magnetic flux of the permanent magnets of themotor 4 is generated". Thus, the d-axis current command value Id* is set to be a negative value. However, in this embodiment, the d-axis current command value Id* is set to be a positive value as shown inFIG. 20 . - Here, as shown in
FIG. 20 , when the frequency is at ωP61, the maximum of the motor voltage modulation rate KhV1 exceeds 1.15 and the minimum exceeds 1.10. As described above, when the KhV1 reaches 1.15, the weakfield control unit 31 switches the FLGweak from OFF to ON; and when the KhV1 decreases to 1.10, the weakfield control unit 31 switches the FLGweak from ON to OFF. Hence, inFIG. 20 where ω1* > ωP61, the weak field control flag FLGweak is kept ON, so that the FLGweak is switched less frequently. - When the inverter frequency command value ω1* further increases and becomes larger than ωP61, a smaller Id* can be used to achieve the KhV1_fil = 1.20. Accordingly, as the ω1* increases, the Id* decreases. If the d-axis current command value Id* arrives at the lower limit (0) and the low range component KhV1_fil of the motor voltage modulation rate exceeds 1.20, Step S164 (see
FIG. 18 ) is judged as "NO". Then, at Step S168, the Id* is set to 0. The frequency ωP62 is referred to as the inverter frequency command value ω1* at which the low range component KhV1_fil of the motor voltage modulation rate starts rising again and is beyond 1.20. - Note that at Step S166 of
FIG. 18 , the d-axis current command value Id* is calculated based on the algorithm ofFIG. 19 . However, like [Expression 10] of the first embodiment, for instance, the d-axis current command value Id* may be calculated by using the proportional gain K in "Id* = (1.20 - KhV1_fil) × K". - According to this embodiment as described above, the d-axis current command unit (32) controls, when the output voltage is lower than the saturation level, the d-axis current command value (Id*) such that a magnetic flux that strengthens a magnetic flux generated by the permanent magnets is generated in the windings.
- This, like the first embodiment, enables the
motor 4 to be driven stably. - [Seventh Embodiment] The following describes how to configure an air conditioner W according to the seventh embodiment of the present invention. In the description below, elements corresponding to the respective elements of
FIGS. 1 to 20 have the same reference numerals so as to avoid redundancy. -
FIG. 21 is a schematic view of the air conditioner W according to the seventh embodiment. As depicted, the air conditioner W includes an indoor unit U1, an outdoor unit U2, a pipe k connecting therebetween, and a remote controller Re. The air conditioner W is an apparatus through which a heat-transfer medium circulates using a well-known heat pump cycle so as to execute air conditioning (e.g., cooling operation, heating operation, dehumidification operation). The remote controller Re is to send or receive various predetermined signals (e.g., to give an operation/stop command, to change a set temperature, to set a timer, to change an operation mode) to or from the indoor unit U1. - The outdoor unit U2 includes an
electronics case 80 that houses various electronics and acompressor 82. Here, theelectronics case 80 includes the converter circuit 2 (seeFIG. 1 ) and the inverter device 3 (seeFIG. 1 ) according to any one of the above first to sixth embodiments. In addition, the inside of thecompressor 82 is provided with the above-describedmotor 4. - Hence, in the air conditioner W according to this embodiment, like the above first to sixth embodiments, the flag FLGweak can be prevented from being switched frequently, which allows for continuously stable operation.
- [Modification Embodiments] The present invention is not limited to the above embodiments, and various modifications are allowed. The above-described embodiments are just examples so as to explain the present invention in an understandable manner. Thus, the present invention is not necessarily limited to embodiments including all the elements described. In addition, part of the configuration of a certain embodiment may be replaced by the configuration of another embodiment. Further, the configuration of a certain embodiment may be added to the configuration of another embodiment. Furthermore, any part of the configuration of each embodiment may be deleted or may be added to or replaced by another configuration. Meanwhile, control lines and/or information lines shown in the drawings indicate what is considered to be necessary for description, so that they may not represent all the control lines and/or information lines required for the products. In fact, almost all the configurations may be connected to one another. Examples of a possible modification regarding the above embodiments include the following.
- (1) Hardware of the
controller 12 according to each embodiment can be realized by a common computer. Thus, any of the programs of the flow charts shown inFIGS. 6 ,9 ,14 ,17 , and18 and table and file information may be stored in storage devices such as a memory, a hard disk, an SSD (solid state drive) or storage media such as an IC card, an SD card, and a DVD, or may be deployed using a communication path. - (2) The processing shown in each of
FIGS. 6 ,9 ,14 ,17 , and18 is described as software processing using a program in each embodiment. However, part or all of them may be replaced by hardware processing using, for example, ASIC (Application Specific Integrated Circuit; IC for a specific purpose) or FPGA (field-programmable gate array). - (3) In addition, the
inverter device 3 according to any one of the first to sixth embodiments may be used for not only the air conditioner W according to the seventh embodiment but also various electric devices such as ventilation fans, freezers, washing machines, cleaners, industrial machines, electric vehicles, railway vehicles, ships, elevators, and escalators. By using the inverter device, these electric devices can exert excellent performance depending on their usage. -
- 3 Inverter device (power conversion device)
- 4 Permanent magnet synchronous motor (motor)
- 9 IPM (inverter)
- 12 Controller
- 24 Speed control unit (q-axis current command unit)
- 31 Weak field control unit
- 32 Weak field change-suppressing control unit (d-axis current command unit)
- 40, 54 Low-pass filter
- 82 Compressor
- ω1* Inverter frequency command value (frequency command value)
- ωP31 Frequency (first command value)
- ωP32 Frequency (second command value)
- Id* d-Axis current command value
- Iq* q-Axis current command value
- Vdc DC voltage detection value
- W Air conditioner
Claims (7)
- A power conversion device comprising:an inverter which converts, in order to drive a motor equipped with a stator having windings and a rotor having permanent magnets, supplied DC voltage to an AC output voltage and supplies the AC output voltage to the windings, wherein, a saturation level at which the output voltage is saturated changes in accordance with the DC voltage; anda controller which, when the output voltage is lower than the saturation level, increases an output current of the inverter to generate in the windings a magnetic flux in such a direction as to weaken or strengthen a magnetic flux generated by the permanent magnets.
- The power conversion device according to claim 1, wherein the controller comprises: when in a coordinate system that rotates at a rotation speed of an electrical angle of the motor, a d-axis is set to a direction of a magnetic flux generated by the permanent magnets and a q-axis is set to an axis orthogonal with the d-axis,
a q-axis current command unit configured to output a q-axis current command value, which is a command value for a q-axis component of the output current, based on a frequency command value; and
a d-axis current command unit configured to output a d-axis current command value, which is a command value for a d-axis component of the output current, based on the frequency command value, wherein
the d-axis current command unit controls, when the output voltage is lower than the saturation level, the d-axis current command value to generate in the windings a magnetic flux in such a direction as to weaken the magnetic flux generated by the permanent magnets. - The power conversion device according to claim 2, wherein the d-axis current command unit controls the d-axis current command value to keep the output voltage substantially constant while the frequency command value changes.
- The power conversion device according to claim 2, wherein the d-axis current command unit sets, when the frequency command value is less than a first command value, the d-axis current command value to 0; increases, when the frequency command value is the first command value or more and less than a predetermined second command value, an absolute value of the d-axis current command value as the frequency command value becomes larger, so as to keep the output voltage substantially constant; and sets, when the frequency command value is the second command value or more, the d-axis current command value to 0.
- The power conversion device according to claim 2, wherein the controller comprises: a low-pass filter into which a value changes in response to a change in the DC voltage is input; and a weak field control unit configured to determine, based on an output signal from the low-pass filter, whether or not weak field control is executed.
- The power conversion device according to claim 1, wherein the controller comprises: when in a coordinate system that rotates at a rotation speed of an electrical angle of the motor, a d-axis is set to a direction of a magnetic flux generated by the permanent magnets and a q-axis is set to an axis orthogonal with the d-axis,
a q-axis current command unit configured to output a q-axis current command value, which is a command value for a q-axis component of the output current, based on a frequency command value; and
a d-axis current command unit configured to output a d-axis current command value, which is a command value for a d-axis component of the output current, based on the frequency command value, wherein
the d-axis current command unit controls, when the output voltage is lower than the saturation level, the d-axis current command value to generate in the windings a magnetic flux in such a direction as to strengthen the magnetic flux generated by the permanent magnets. - An air conditioner comprising:a compressor having a motor equipped with a stator having windings and a rotor having permanent magnets;an inverter which converts supplied DC voltage to an AC output voltage and supplies the AC output voltage to the windings, wherein a saturation level at which the output voltage is saturated, changes in accordance with the DC voltage; anda controller which, when the output voltage is lower than the saturation level, increases an output current of the inverter to generate in the windings a magnetic flux in such a direction as to weaken or strengthen a magnetic flux generated by the permanent magnets.
Applications Claiming Priority (2)
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JP2016215919A JP6827297B2 (en) | 2016-11-04 | 2016-11-04 | Power converter and air conditioner |
PCT/JP2017/038401 WO2018084027A1 (en) | 2016-11-04 | 2017-10-24 | Power conversion device and air conditioner |
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EP3422553A4 EP3422553A4 (en) | 2019-10-09 |
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EP (1) | EP3422553A4 (en) |
JP (1) | JP6827297B2 (en) |
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US10998834B2 (en) * | 2017-08-21 | 2021-05-04 | Mitsubishi Electric Corporation | Power conversion device and electric power steering device |
WO2020059108A1 (en) * | 2018-09-21 | 2020-03-26 | 三菱電機株式会社 | Inverter control device |
CN111756302B (en) * | 2019-03-29 | 2022-06-17 | 安川电机(中国)有限公司 | Method, device and equipment for controlling output voltage of frequency converter and vacuum system |
WO2021226104A1 (en) * | 2020-05-06 | 2021-11-11 | Watlow Electric Manufacturing Company | Isolated power converter for a thermal system |
CN112688610B (en) * | 2021-03-22 | 2021-06-11 | 浙大城市学院 | Vector flux weakening control method for vehicle permanent magnet synchronous motor |
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JP3971979B2 (en) * | 2002-09-13 | 2007-09-05 | 日立アプライアンス株式会社 | Air conditioner |
US7545056B2 (en) | 2003-05-27 | 2009-06-09 | Pratt & Whitney Canada Corp. | Saturation control of electric machine |
US7262539B2 (en) | 2004-11-26 | 2007-08-28 | Pratt & Whitney Canada Corp. | Saturation control of electric machine |
US6965183B2 (en) | 2003-05-27 | 2005-11-15 | Pratt & Whitney Canada Corp. | Architecture for electric machine |
US7583063B2 (en) | 2003-05-27 | 2009-09-01 | Pratt & Whitney Canada Corp. | Architecture for electric machine |
US7304451B2 (en) * | 2004-03-17 | 2007-12-04 | Kabushiki Kaisha Yasakawa Denki | Motor control apparatus and method for generating modulation wave instruction of PWM inverter of the same motor control apparatus |
JP4677852B2 (en) * | 2005-08-11 | 2011-04-27 | 株式会社日立製作所 | Vector controller for permanent magnet synchronous motor |
JP4466600B2 (en) * | 2006-03-31 | 2010-05-26 | アイシン・エィ・ダブリュ株式会社 | Electric drive control device and electric drive control method |
JP5257365B2 (en) | 2007-11-15 | 2013-08-07 | 株式会社安川電機 | Motor control device and control method thereof |
JP5325556B2 (en) | 2008-12-12 | 2013-10-23 | 日立アプライアンス株式会社 | Motor control device |
CN101714770B (en) * | 2009-12-16 | 2013-10-02 | 中国科学院上海微***与信息技术研究所 | Field high efficiency wind and solar generation system and method |
JP5633640B2 (en) | 2011-04-21 | 2014-12-03 | 日産自動車株式会社 | Electric motor control device and electric motor control method |
JP6293401B2 (en) | 2011-12-28 | 2018-03-14 | 三菱重工サーマルシステムズ株式会社 | Motor controller for air conditioner and air conditioner |
JP6011324B2 (en) * | 2012-12-26 | 2016-10-19 | アイシン・エィ・ダブリュ株式会社 | Rotating electrical machine control device |
JP5717808B2 (en) | 2013-07-18 | 2015-05-13 | ファナック株式会社 | Current control device for synchronous motor |
JP5968564B2 (en) * | 2014-07-30 | 2016-08-10 | 三菱電機株式会社 | Power converter |
JP6497895B2 (en) * | 2014-11-17 | 2019-04-10 | シャープ株式会社 | Control device for synchronous motor |
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US10680544B2 (en) | 2020-06-09 |
CN109155606A (en) | 2019-01-04 |
CN109155606B (en) | 2020-03-17 |
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